

=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.Prototype 3810001
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=3810001
atc_id=3810001


[General]
performance=The Antonov An-38 is a stretched and upgraded version of Antonov's earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kiev, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019 
atc_type=Antonov 
atc_model=An-38-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=11.6, -1.2, 3.2       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 20943.91
empty_weight = 11023.11
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.49, 36.32, 5.09, fx_navgrem
light.1 = 3, -1.50, -36.31, 4.98, fx_navredm
light.2 = 4, 12.11, -1.35, 4.17, fx_vclight_yellow
light.3 = 4, 12.24, 1.37, 4.21, fx_vclight_yellow
light.4 = 4, 12.20, 0, 4.19, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -28.39, -8.5, 9.99, fx_beaconb
light.7 = 2, -26.94, 8.31, 0.45, fx_beaconh
light.8 = 7, -2.02, 9.2, 1.68, fx_737NG
light.9 = 7, -2.17, -9.2, 1.63, fx_737NG
light.10 = 3, -31.19, 0, 4.82, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 5.9, -9.15, 4.1,
engine.1 = 5.9, 9.15, 4.1,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -2.5
static_cg_height = 4.1
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 17.3822, 0, -4.1221, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 3, 10, 0, 400, 400
point.1 = 1, -3.3877, -5.5, -4.5875, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 2, 400, 400
point.2 = 1, -3.3855, 5.5, -4.6578, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 550.54
wing_span = 72.37
wing_root_chord = 6.19
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 4
wing_pos_apex_lon = 2.40
wing_pos_apex_vert = 4.48
htail_area = 95
htail_span = 16.86
htail_pos_lon = -23.92
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 10
vtail_area = 157.64
vtail_span = 5.34
vtail_sweep = 35
vtail_pos_lon = -24.30
vtail_pos_vert = 5.15
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.Prototype 3810001
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=3810001
atc_id=3810001

[General]
performance=The Antonov An-38 is a stretched and upgraded version of Antonov's earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kiev, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019 
atc_type=Antonov 
atc_model=An-38-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=11.6, -1.2, 3.2       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 20943.91
empty_weight = 11023.11
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.49, 36.32, 5.09, fx_navgrem
light.1 = 3, -1.50, -36.31, 4.98, fx_navredm
light.2 = 4, 12.11, -1.35, 4.17, fx_vclight_yellow
light.3 = 4, 12.24, 1.37, 4.21, fx_vclight_yellow
light.4 = 4, 12.20, 0, 4.19, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -28.39, -8.5, 9.99, fx_beaconb
light.7 = 2, -26.94, 8.31, 0.45, fx_beaconh
light.8 = 7, -2.02, 9.2, 1.68, fx_737NG
light.9 = 7, -2.17, -9.2, 1.63, fx_737NG
light.10 = 3, -31.19, 0, 4.82, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 5.9, -9.15, 4.1,
engine.1 = 5.9, 9.15, 4.1,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 3, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 550.54
wing_span = 72.37
wing_root_chord = 6.19
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 4
wing_pos_apex_lon = 2.40
wing_pos_apex_vert = 4.48
htail_area = 95
htail_span = 16.86
htail_pos_lon = -23.92
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 10
vtail_area = 157.64
vtail_span = 5.34
vtail_sweep = 35
vtail_pos_lon = -24.30
vtail_pos_vert = 5.15
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.Prototype 3810001
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=3810001
atc_id=3810001

[General]
performance=The Antonov An-38 is a stretched and upgraded version of Antonov's earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kiev, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019 
atc_type=Antonov 
atc_model=An-38-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=11.6, -1.2, 3.2       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 20943.91
empty_weight = 11023.11
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.49, 36.32, 5.09, fx_navgrem
light.1 = 3, -1.50, -36.31, 4.98, fx_navredm
light.2 = 4, 12.11, -1.35, 4.17, fx_vclight_yellow
light.3 = 4, 12.24, 1.37, 4.21, fx_vclight_yellow
light.4 = 4, 12.20, 0, 4.19, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -28.39, -8.5, 9.99, fx_beaconb
light.7 = 2, -26.94, 8.31, 0.45, fx_beaconh
light.8 = 7, -2.02, 9.2, 1.68, fx_737NG
light.9 = 7, -2.17, -9.2, 1.63, fx_737NG
light.10 = 3, -31.19, 0, 4.82, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 5.9, -9.15, 4.1,
engine.1 = 5.9, 9.15, 4.1,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 3, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 0, 0, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 550.54
wing_span = 82.29
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 4
wing_pos_apex_lon = 2.40
wing_pos_apex_vert = 4.48
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 10
vtail_area = 157.64
vtail_span = 5.34
vtail_sweep = 35
vtail_pos_lon = -25.96
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.Prototype 3810001
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=3810001
atc_id=3810001

[General]
performance=The Antonov An-38 is a stretched and upgraded version of Antonov's earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kiev, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019 
atc_type=Antonov 
atc_model=An-38-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 20943.91
empty_weight = 11023.11
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.49, 36.32, 5.09, fx_navgrem
light.1 = 3, -1.50, -36.31, 4.98, fx_navredm
light.2 = 4, 12.11, -1.35, 4.17, fx_vclight_yellow
light.3 = 4, 12.24, 1.37, 4.21, fx_vclight_yellow
light.4 = 4, 12.20, 0, 4.19, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -28.39, -8.5, 9.99, fx_beaconb
light.7 = 2, -26.94, 8.31, 0.45, fx_beaconh
light.8 = 7, -2.02, 9.2, 1.68, fx_737NG
light.9 = 7, -2.17, -9.2, 1.63, fx_737NG
light.10 = 3, -31.19, 0, 4.82, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 5.9, -9.15, 4.1,
engine.1 = 5.9, 9.15, 4.1,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 550.54
wing_span = 82.29
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 4
wing_pos_apex_lon = 2.40
wing_pos_apex_vert = 4.48
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 10
vtail_area = 157.64
vtail_span = 5.34
vtail_sweep = 35
vtail_pos_lon = -25.96
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.Prototype 3810001
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=3810001
atc_id=3810001

[General]
performance=The Antonov An-38 is a stretched and upgraded version of Antonov's earlier An-28. It is a twin-engined turboprop transport aircraft, designed by the Antonov Design Bureau in Kiev, Ukraine. Production is in Novosibirsk, Russia, but some crucial parts are also made in Ukraine and Belarus. It first flew in 1994, and received international flight certification in April 2000. A total of 11 were built and 2 remain in airline service as of August 2019 
atc_type=Antonov 
atc_model=An-38-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399,39
empty_weight = 28241,22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -1.49, 36.32, 5.09, fx_navgrem
light.1 = 3, -1.50, -36.31, 4.98, fx_navredm
light.2 = 4, 12.11, -1.35, 4.17, fx_vclight_yellow
light.3 = 4, 12.24, 1.37, 4.21, fx_vclight_yellow
light.4 = 4, 12.20, 0, 4.19, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -28.39, -8.5, 9.99, fx_beaconb
light.7 = 2, -26.94, 8.31, 0.45, fx_beaconh
light.8 = 7, -2.02, 9.2, 1.68, fx_737NG
light.9 = 7, -2.17, -9.2, 1.63, fx_737NG
light.10 = 3, -31.19, 0, 4.82, fx_navwhi

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 5.9, -9.15, 4.1,
engine.1 = 5.9, 9.15, 4.1,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 1.5, fx_landing
light.15 = 8, 3.5, 4.6, 1.5, fx_landing
light.16 = 9, -19.37, -0.7, 9.22, fx_landing
light.17 = 9, -19.37, 0.7, 9.22, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3, 
engine.1 = 8, 13.22, 7.3, 

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 1.5, fx_landing
light.15 = 8, 3.5, 4.6, 1.5, fx_landing
light.16 = 9, -19.37, -1, 9.22, fx_landing
light.17 = 9, -19.37, 1, 9.22, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 1.5, fx_landing
light.15 = 8, 3.5, 4.6, 1.5, fx_landing
light.16 = 9, -19.37, -1.3, 9.25, fx_landing
light.17 = 9, -19.37, 1.3, 9.25, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 2, fx_landing
light.15 = 8, 3.5, 4.6, 2, fx_landing
light.16 = 9, -19.37, -1.5, 9.25, fx_landing
light.17 = 9, -19.37, 1.5, 9.25, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 1.5, fx_landing
light.15 = 8, 3.5, 4.6, 1.5, fx_landing
light.16 = 9, -19.37, -0.7, 9.22, fx_landing
light.17 = 9, -19.37, 0.7, 9.22, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -4.6, 1.5, fx_landing
light.15 = 8, 3.5, 4.6, 1.5, fx_landing
light.16 = 9, -19.37, -1, 9.4, fx_landing
light.17 = 9, -19.37, 1, 9.4, fx_landing

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=9.19 
propeller_blades=5 
propeller_moi=28.000 //19.000
beta_max=79.500 
beta_min=2.500 
min_gov_rpm=14000.000 //17000
prop_tc=0.004 
gear_reduction_ratio=19.072 
fixed_pitch_beta=20.000 //20
low_speed_theory_limit=80.000 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=900 
beta_feather=82.000 
power_absorbed_cf=0.900 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=2.500 //10
minimum_reverse_beta=-15.000  //-21
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.040 // 0.040
inlet_area=1 
rated_N2_rpm=29600.000  //36660 
static_thrust=30.000 
afterburner_available=0 

[turboprop_engine]
maximum_torque=5008.800 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 95
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 38.75
aileron_area = 16.15
rudder_area = 40
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 19
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0                   
propeller_type=0                     
propeller_diameter=12.2              
propeller_blades=6                     
propeller_moi=76                  
beta_max=44                   
beta_min=9                   
min_gov_rpm=12000                
prop_tc=0.0024                 
gear_reduction_ratio=12.5                  
fixed_pitch_beta=0                     
low_speed_theory_limit=81                   
prop_sync_available=1                    
prop_deice_available=1                     
prop_feathering_available=1                    
prop_auto_feathering_available=1               
min_rpm_for_feather=398                  
beta_feather=79.2                  
power_absorbed_cf=0.9                  
defeathering_accumulators_available=0          
prop_reverse_available=0.1                    
minimum_on_ground_beta=0.1                  
minimum_reverse_beta=-0.1                
rotation=1,1

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000  //36660 
static_thrust=198.000 
afterburner_available=1

[turboprop_engine]
maximum_torque=12091.00 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.1, 0, 0
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 30

station_load.0 = 176.37, 11.82, -1.10, 0.94
station_load.1 = 176.37, 11.87, 1.10, 0.94
station_load.2 = 165.35, 9, -1.7, 1
station_load.3 = 165.35, 9, 1.7, 1
station_load.4 = 165.35, 6.6, -1.7, 1
station_load.5 = 165.35, 6.6, 1.7, 1
station_load.6 = 165.35, 6.6, 0, 1
station_load.7 = 165.35, 4.14, 1.7, 1
station_load.8 = 165.35, 4.08, 0, 1
station_load.9 = 165.35, 4.2, -1.7, 1
station_load.10 = 165.35, 1.8, -1.7, 1
station_load.11 = 165.35, 1.8, 1.7, 1
station_load.12 = 165.35, 1.8, 0, 1
station_load.13 = 165.35, -0.6, -1.7, 1
station_load.14 = 165.35, -0.6, 1.7, 1
station_load.15 = 165.35, -0.6, 0, 1
station_load.16 = 165.35, -3, 1.7, 1.17
station_load.17 = 165.35, -3, 0, 1
station_load.18 = 165.35, -3, -1.7, 1
station_load.19 = 165.35, -5.4, -1.7, 1
station_load.20 = 400, -16.65, -0.05, 0
station_load.21 = 165.35, -5.4, 0, 1
station_load.22 = 165.35, -5.4, 1.7, 1
station_load.23 = 165.35, -7.8, -1.7, 1
station_load.24 = 165.35, -7.8, 0, 0
station_load.25 = 165.35, -7.8, 1.7, 1
station_load.26 = 165.35, -10.2, -1.7, 1
station_load.27 = 165.35, -10.2, 0, 1
station_load.28 = 165.35, -10.2, 1.7, 1
station_load.29 = 165.35, -12.6, 0, 1


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftAux = -1, -22, 5, 239.08, 5
RightAux = -1, 22, 5, 239.08, 5
RightTip = -1, 0, 5, 258.89, 5


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=44 
beta_min=9 
min_gov_rpm=12000 
prop_tc=0.0024 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=81 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=398 
beta_feather=79.2 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=0.1 
minimum_on_ground_beta=0.1 
minimum_reverse_beta=-0.1 
rotation=1,1

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000  //36660 
static_thrust=198.000 
afterburner_available=1 

[turboprop_engine]
maximum_torque=12091.00 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 19900
empty_weight_roll_MOI = 17900
empty_weight_yaw_MOI = 29900
empty_weight_coupled_MOI = 0
max_number_of_stations = 4

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=44 
beta_min=9 
min_gov_rpm=12000 
prop_tc=0.0024 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=81 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=398 
beta_feather=79.2 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=0.1 
minimum_on_ground_beta=0.1 
minimum_reverse_beta=-0.1 
rotation=1,1

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000  //36660 
static_thrust=198.000 
afterburner_available=1 

[turboprop_engine]
maximum_torque=12091.00 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 750000
empty_weight_roll_MOI = 650000
empty_weight_yaw_MOI = 600000
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=2.5 
aileron_effectiveness=1.3 
rudder_effectiveness=1.5 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=44 
beta_min=9 
min_gov_rpm=12000 
prop_tc=0.0024 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=81 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=398 
beta_feather=79.2 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=0.1 
minimum_on_ground_beta=0.1 
minimum_reverse_beta=-0.1 
rotation=1,1

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000  //36660 
static_thrust=198.000 
afterburner_available=1 

[turboprop_engine]
maximum_torque=12091.00 //2830.800
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 10.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140_38
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 750000
empty_weight_roll_MOI = 400000
empty_weight_yaw_MOI = 600000
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]  // completed
cruise_lift_scalar=1.5
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=0.8 
pitch_stability=2.0 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=2.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
hi_alpha_on_yaw          = 1.0   
p_factor_on_yaw          = 0.5      
torque_on_roll           = 0.5         
gyro_precession_on_yaw   = 6.5          
gyro_precession_on_pitch = 6.5     
gyro_precession_on_roll  = 2.5 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=44 
beta_min=9 
min_gov_rpm=12000 
prop_tc=0.0024 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=81 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=398 
beta_feather=79.2 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=0.1 
minimum_on_ground_beta=0.1 
minimum_reverse_beta=-0.1 
rotation=1,1

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=13750.000  //15000 
static_thrust=198.000 
afterburner_available=1 

[turboprop_engine]
maximum_torque=11774.21 //12091.00
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.480000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.500
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1
parasite_drag_scalar=0.65
induced_drag_scalar=1.3
elevator_effectiveness=0.8
aileron_effectiveness=0.9
rudder_effectiveness=1.0
pitch_stability=1.2
roll_stability=1.2
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76
beta_max=50.0
beta_min=3
min_gov_rpm=12000 
prop_tc=0.1
gear_reduction_ratio=12.5 
fixed_pitch_beta=0
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 


[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.800
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.15, 2.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.3 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.800
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 2645.55, 12, 0, 3
station_load.1 = 2645.55, 6, 0, 3
station_load.2 = 2645.55, 0, 0, 3
station_load.3 = 2645.55, -6, 0, 3
station_load.4 = 2645.55, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.3 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.800
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 4
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, -1.6589, -36.5261, 4.8563, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.644, 36.423, 4.8738, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -26.9523, -8.5158, 0.2525, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 19.4011, 0, 0.0456, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -27.0208, 8.4678, 0.1561, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -32.1346, -8.5431, 4.7976, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 8.4671, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 6.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 4.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 4
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 0.0604, 0, -1.819, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 6.6
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 4
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1.5
static_cg_height = 2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1.5
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1.5
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = 0
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 1.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.65, 2.2, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 2, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.5, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.5, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 2, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.8, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.8, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.2, 1600, 0, 1, 17, 0.3, 2, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.3, 2, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.2, 2, 0.3, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.65, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.15, 2, 0.2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.3, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.3, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.15, 1.2, 0.2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.6, 2.5, 0.8, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.6, 2.5, 0.8, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.15, 2.5, 0.5, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.1, 1600, 0, 1, 17, 0.15, 1.6, 0.2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.7, 2.5, 0.6, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 2.2, 0.6, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 0.2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 1.6, 1.5, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.3, 2.6, 2.5, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.15, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4937, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4902, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.4, 1.2, 0.7, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.4, 1.2, 1, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.4, 1.2, 1, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.2
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 2.5
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.4, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.5, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.5, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1.3, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.9, 1600, 1, 1.3, 0, 0.5, 1.2, 1.3, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.9, 1600, 2, 1.3, 0, 0.5, 1.2, 1.3, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.95, 1600, 1, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.95, 1600, 2, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 2.6, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 1.6, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 1, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.5, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 1, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.7, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.3, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.3, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.3, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.6, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.1, 1600, 1, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.1, 1600, 2, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4.2, 1600, 1, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4.2, 1600, 2, 1.3, 0, 0.65, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -4, 1600, 1, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -4, 1600, 2, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.0881, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.5, 1600, 1, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.5, 1600, 2, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.55, 1.2, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.55, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.55, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.6, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.6, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.3, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.4, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.4, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=F27_MK100
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.6, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.6, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.900
drag_scalar= 1.000  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.85, -1.98, 5.46, fx_vclight_yellow
light.3 = 4, 22.81, 1.94, 5.63, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000




=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.20, -1.98, 5.54, fx_vclight_yellow
light.3 = 4, 23.20, 1.93, 5.53, fx_vclight_yellow
light.4 = 4, 21.32, -0.01, 5.61, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.20, -1.98, 5.92, fx_vclight_yellow
light.3 = 4, 23.17, 1.93, 5.92, fx_vclight_yellow
light.4 = 4, 23.84, 0, 5.16, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.26, -2.75, 5.92, fx_vclight_yellow
light.3 = 4, 23.13, 2.79, 5.92, fx_vclight_yellow
light.4 = 4, 23.18, 0, 5.90, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.86, -2.02, 5.92, fx_vclight_yellow
light.3 = 4, 22.93, 1.97, 5.92, fx_vclight_yellow
light.4 = 4, 22.85, 0, 5.90, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.90, -1.98, 5.92, fx_vclight_yellow
light.3 = 4, 23.91, 1.91, 5.92, fx_vclight_yellow
light.4 = 4, 23.82, 0, 5.90, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.97, -1.98, 5.30, fx_vclight_yellow
light.3 = 4, 23.96, 1.91, 5.31, fx_vclight_yellow
light.4 = 4, 23.99, 0, 5.29, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.94, -1.30, 5.30, fx_vclight_yellow
light.3 = 4, 23.98, 1.30, 5.30, fx_vclight_yellow
light.4 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.5 = 2, -6.31, 0, 9.58, fx_beaconb
light.6 = 2, 1.09, 0, -0.86, fx_beaconh
light.7 = 7, -0.2, 13.3, 4.7, fx_737NG
light.8 = 7, -0.2, -13.3, 4.7, fx_737NG
light.9 = 5, 27.21, -2.13, -0.17, fx_landing
light.10 = 5, 27.21, 2.16, -0.18, fx_landing
light.11 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.12 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.13 = 8, 3.5, -5, 2.2, Yk42_wing
light.14 = 8, 3.5, 5, 2.2, Yk42_wing
light.15 = 9, -19.37, -1, 9.4, VM742_logo
light.16 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 24.01, 0.01, 5.30, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.03, 0.01, 5.10, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 22.98, 0.01, 5.36, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.65, 0.01, 5.33, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 24.20, 0.01, 5.22, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0.01, 5.22, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.15, 0.01, 5.31, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.26, 0.01, 5.86, fx_vclight_yellow
light.3 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.4 = 2, -6.31, 0, 9.58, fx_beaconb
light.5 = 2, 1.09, 0, -0.86, fx_beaconh
light.6 = 7, -0.2, 13.3, 4.7, fx_737NG
light.7 = 7, -0.2, -13.3, 4.7, fx_737NG
light.8 = 5, 27.21, -2.13, -0.17, fx_landing
light.9 = 5, 27.21, 2.16, -0.18, fx_landing
light.10 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.11 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.26, 0.01, 5.86, fx_vclight_yellow
light.3 = 4, 23.33, -2.04, 5.77, fx_vclight_yellow
light.4 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.5 = 2, -6.31, 0, 9.58, fx_beaconb
light.6 = 2, 1.09, 0, -0.86, fx_beaconh
light.7 = 7, -0.2, 13.3, 4.7, fx_737NG
light.8 = 7, -0.2, -13.3, 4.7, fx_737NG
light.9 = 5, 27.21, -2.13, -0.17, fx_landing
light.10 = 5, 27.21, 2.16, -0.18, fx_landing
light.11 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.12 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.13 = 8, 3.5, -5, 2.2, Yk42_wing
light.14 = 8, 3.5, 5, 2.2, Yk42_wing
light.15 = 9, -19.37, -1, 9.4, VM742_logo
light.16 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.26, 0.01, 5.86, fx_vclight_yellow
light.3 = 4, 22.81, -2.04, 6.04, fx_vclight_yellow
light.4 = 4, 22.81, 1.94, 6.05, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.16, 0, 6.02, fx_vclight_yellow
light.3 = 4, 22.81, -2.04, 6.04, fx_vclight_yellow
light.4 = 4, 22.81, 1.94, 6.05, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 191712
empty_weight_roll_MOI = 76538
empty_weight_yaw_MOI = 129316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.28, 0, 5.63, fx_vclight_yellow
light.3 = 4, 23.26, -2.03, 5.62, fx_vclight_yellow
light.4 = 4, 23.28, 1.94, 5.60, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=1.1 
parasite_drag_scalar=0.65 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700
drag_scalar= 1.300  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.22, 7.3,
engine.1 = 8, 13.22, 7.3,
engine.2 = -33, 0, 5.5, 

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -11, 7.3, 
engine.1 = 8, 15.44, 7.3, 
engine.2 = -33, 0, 5.5, 

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -11, 7.3, 
engine.1 = 8, 15.6, 7.3, 
engine.2 = -33, 0, 5.5, 

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -12, 7.3, 
engine.1 = 8, 14.6, 7.3, 
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3, 
engine.1 = 8, 13.3, 7.3, 
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 17, 0.1, 0.2, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.3, 0.4, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 0.4, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 0.6, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 0.6, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 0.3, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 0.3, 1, 10, 10, 0, 400, 400
point.1 = 1, -2.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.1, 0.7, 1, 10, 10, 0, 400, 400
point.1 = 1, -2.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.1, 0.4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -2.5993, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2.583, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.1, 0.4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 0.7, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 0.7, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 1, 2, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.3, 1, 1, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.3, 1.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.3, 2.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 2.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 2.6, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -2, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 2, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -2, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 3, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -2, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -2, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 3, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 3, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 1.5, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 1.5, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.2, 3, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 1, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 1, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 3.5, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 3
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 8
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 11, 0, 3
station_load.1 = 1891.57, 5, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 13, 0, 3
station_load.1 = 1891.57, 7, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = -2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 2
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 380712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 4.5
htail_incidence = 4
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300
drag_scalar= 1.600  // 1.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 548.95
wing_span = 83.66
wing_root_chord = 9.49
wing_dihedral = 1
wing_incidence = 2
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 185.461
htail_span = 30.09
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 157.64
vtail_span = 14.77
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 55.54
aileron_area = 33
rudder_area = 54
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.5 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 40, 0.15, 4, 0.7, 10, 10, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 10, 10, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 10, 10, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 30
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.5 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 16.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 0.700   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.21, -2.13, -0.17, fx_landing
light.11 = 5, 27.21, 2.16, -0.18, fx_landing
light.12 = 6, 27.23, -2.10, -0.28, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 55, 0.15, 4, 0.7, 12, 12, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 15, 15, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 15, 15, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 15
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 30.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.20, -2.13, -0.32, fx_landing
light.11 = 5, 27.20, 2.16, -0.33, fx_landing
light.12 = 6, 27.21, -2.09, -0.32, fx_taxi_an24
light.13 = 6, 27.22, 2.14, -0.33, fx_taxi_an24
light.14 = 8, 3.5, -5, 2.2, Yk42_wing
light.15 = 8, 3.5, 5, 2.2, Yk42_wing
light.16 = 9, -19.37, -1, 9.4, VM742_logo
light.17 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.005
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 55, 0.15, 4, 0.7, 12, 12, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 15, 15, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 15, 15, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 15
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.9 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 30.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.20, -2.13, -0.32, fx_landing
light.11 = 5, 27.20, 2.16, -0.33, fx_landing
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.30
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 55, 0.15, 4, 0.7, 12, 12, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 15, 15, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 15, 15, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 15
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.8 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1   
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 30.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.20, -2.13, -0.32, fx_landing
light.11 = 5, 27.20, 2.16, -0.33, fx_landing
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.30
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 55, 0.15, 4, 0.7, 12, 12, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 15, 15, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 15, 15, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 15
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,0
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.8 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 30.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000



=*=*=*=*=*=    BACKUP    =*=*=*=*=*=    SICHERUNG    =*=*=*=*=*=

[fltsim.0]
title=Antonov An-140-100
sim=An140v03
model=
panel=
sound=
texture=
kb_checklists=
atc_airline=
ui_manufacturer=OKB Antonov
ui_type=Antonov An-140-100
ui_variation=01.VVS RF 08851
description=Antonov An-140-100
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
atc_flight_number=08851
atc_id=08851

[General]
performance=The Antonov An-140 is a turboprop regional airliner, designed by the Ukrainian Antonov ASTC bureau as a successor to the Antonov An-24, with extended cargo capacity and the ability to use unprepared airstrips. 
The AN-140-100 aircraft differs from the basic version with the larger wingspan. Can be built for civilian, military and special purpose: maritime patrol, medical, aerial photography, geological exploration, freight etc 
atc_type=Antonov 
atc_model=An-140-100 
prop_anim_ratio=1.76
editable=1 

[Views]
eyepoint=23.5, -2.0, 5.8       //(feet) longitudinal, lateral, vertical distance from reference datum

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47399.39
empty_weight = 28241.22
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 6
empty_weight_pitch_MOI = 680712
empty_weight_roll_MOI = 210538
empty_weight_yaw_MOI = 390316
empty_weight_coupled_MOI = 0
max_number_of_stations = 5

station_load.0 = 1891.57, 12, 0, 3
station_load.1 = 1891.57, 6, 0, 3
station_load.2 = 1891.57, 0, 0, 3
station_load.3 = 1891.57, -6, 0, 3
station_load.4 = 1891.57, -12, 0, 3


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, 2, 41.1, 9.6, fx_navgrem
light.1 = 3, 2, -41.1, 9.6, fx_navredm
light.2 = 4, 23.55, 0, 5.38, fx_vclight_yellow
light.3 = 4, 23.55, -2.03, 5.41, fx_vclight_yellow
light.4 = 4, 23.56, 1.94, 5.40, fx_vclight_yellow
light.5 = 10, -2.09, 0, 4.00, fx_vclight_yellow
light.6 = 2, -6.31, 0, 9.58, fx_beaconb
light.7 = 2, 1.09, 0, -0.86, fx_beaconh
light.8 = 7, -0.2, 13.3, 4.7, fx_737NG
light.9 = 7, -0.2, -13.3, 4.7, fx_737NG
light.10 = 5, 27.20, -2.13, -0.32, fx_landing
light.11 = 5, 27.20, 2.16, -0.33, fx_landing
light.12 = 8, 3.5, -5, 2.2, Yk42_wing
light.13 = 8, 3.5, 5, 2.2, Yk42_wing
light.14 = 9, -19.37, -1, 9.4, VM742_logo
light.15 = 9, -19.37, 1, 9.4, VM742_logo

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.30
min_throttle_limit = -0.25
max_contrail_temperature = -39.0
engine.0 = 8, -13.3, 7.3,
engine.1 = 8, 13.3, 7.3,
engine.2 = -33, 0, 5.5,

[smokesystem]
smoke.0 = 1.79, -2.01, 9.2, fx_smoke_rx
smoke.1 = 1.76, -2.03, -9.2, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 3
electric_pump = 1

LeftMain = 0, -22, 9, 724.03, 10
RightMain = 0, 22, 9, 724.03, 10


[contact_points]
static_pitch = -1
static_cg_height = 3
tailwheel_lock = 0
gear_system_type = 4
max_number_of_points = 12

point.0 = 1, 24.4822, 0, -3.3, 1600, 0, 1, 55, 0.15, 4, 0.7, 12, 12, 0, 400, 400
point.1 = 1, -1.6, -5.5, -3.7, 1600, 1, 1.3, 0, 0.7, 0.7, 1.4, 15, 15, 2, 400, 400
point.2 = 1, -1.6, 5.5, -3.7, 1600, 2, 1.3, 0, 0.7, 0.8, 1.4, 15, 15, 3, 400, 400
point.3 = 2, 0.8, -42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.8, 42, 9.5, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -12.8598, 0, -0.4428, 2360.907, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 2.1877, 0, -0.8379, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, 11.6675, 0, -0.6637, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2, -37.6145, 0, 4.5743, 1574.803, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, 32.8019, 0, 1.9532, 0, 0, 22, 0.3, 2.5, 0.7, 4, 4, 4, 9, 0, 0
point.10 = 2, -32.0914, 0, 4.8411, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.11 = 2, -6.5267, 0, -0.7933, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0


[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0.0362,0.0362,0.0362,1.5288,0.7645,0.7645,0.0425,1.4986,1.3121,1.3121
//ACM_AREAW2// 0.0487,1.4500,1.8782,1.8782,0.0732,1.4019,2.4437,2.4437,0.0974,1.3536
//ACM_AREAW3// 3.0276,3.0276,0.1224,1.2869,3.5931,3.5931,0.1650,1.2752,4.3765,4.3765
//ACM_AREAW4// 0.1712,1.2266,5.2504,5.2504,0.2140,1.1785,6.5057,6.5057,0.3837,1.0575
//ACM_AREAH1// 0.0362,0.0362,0,1.1584,0.2655,0.2655,0.0390,1.1236,0.4864,0.4864
//ACM_AREAH2// 0.0847,1.1267,0.6951,0.6951,0.1368,1.1232,1.0132,1.0132,0.2236,1.1186
//ACM_AREAH3// 1.2401,1.2401,0.2829,1.0994,1.4579,1.4579,0.3287,1.1009,1.6267,1.6267
//ACM_AREAH4// 0.3745,1.1002,1.8085,1.8085,0.4338,1.1081,2.0422,2.0422,0.5066,1.0937
//ACM_AREAV1// 0,0,0,3.1789,0.3531,0.3531,0.2860,3.2107,0.7063,0.7063
//ACM_AREAV2// 0.5720,3.2423,1.0592,1.0592,0.8579,3.2741,1.4127,1.4127,1.1440,3.3059
//ACM_AREAV3// 1.7661,1.7661,1.4299,3.3375,2.1191,2.1191,1.7158,3.3691,2.4725,2.4725
//ACM_AREAV4// 2.0020,3.4010,2.8257,2.8257,2.2883,3.4326,3.1789,3.1789,2.5743,3.4644
//ACM_CAREAW1// 4.9949,4.9949,1.4644,1.9730,5.5499,5.5499,1.4857,1.9693,6.1048,6.1048
//ACM_CAREAW2// 1.5068,1.9651,6.6598,6.6598,1.5283,1.9608,7.2147,7.2147,1.5497,1.9569
//ACM_CAREAW3// 7.7698,7.7698,1.5707,1.9527,8.3247,8.3247,1.5923,1.9486,8.8795,8.8795
//ACM_CAREAW4// 1.6136,1.9443,9.4348,9.4348,1.6346,1.9400,9.9898,9.9898,1.6562,1.9362
//ACM_CAREAH1// 0,0,1.1236,2.2472,0.3745,0.3745,1.1828,2.2504,0.7491,0.7491
//ACM_CAREAH2// 1.2423,2.2534,1.1236,1.1236,1.3013,2.2567,1.4982,1.4982,1.3609,2.2599
//ACM_CAREAH3// 1.8724,1.8724,1.4203,2.2630,2.2472,2.2472,1.4795,2.2662,2.6219,2.6219
//ACM_CAREAH4// 1.5389,2.2692,2.9965,2.9965,1.5980,2.2725,3.3710,3.3710,1.6576,2.2755
//ACM_CAREAV1// 0,0,0.7947,2.3842,0.3531,0.3531,1.0808,2.5431,0.7063,0.7063
//ACM_CAREAV2// 1.3667,2.7019,1.0592,1.0592,1.6526,2.8608,1.4127,1.4127,1.9385,3.0197
//ACM_CAREAV3// 1.7661,1.7661,2.2249,3.1786,2.1191,2.1191,2.5109,3.3375,2.4725,2.4725
//ACM_CAREAV4// 2.7969,3.4964,2.8257,2.8257,3.0829,3.6552,3.1789,3.1789,3.3691,3.8141
wing_area = 606.65
wing_span = 83.68
wing_root_chord = 9.71
wing_dihedral = 1
wing_incidence = 1
wing_twist = -2
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2
wing_pos_apex_vert = 9
htail_area = 184
htail_span = 29.94
htail_pos_lon = -26.59
htail_pos_vert = 7.22
htail_incidence = 4
htail_sweep = 15
vtail_area = 132.82
vtail_span = 15.72
vtail_sweep = 35
vtail_pos_lon = -25.95
vtail_pos_vert = 7.94
elevator_area = 56.2
aileron_area = 34
rudder_area = 39.5
elevator_up_limit = 15
elevator_down_limit = 15
aileron_up_limit = 22
aileron_down_limit = 16
rudder_limit = 25
elevator_trim_limit = 20
spoiler_limit = 53
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 26
generator_alternator_voltage = 27
max_generator_alternator_amps = 250
engine_generator_map = 1,1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 100, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 1
auto_feather = 0, 15, 17
hydraulic_pump = 0, 2, 17
fuel_transfer_pump = 0, 5, 17
propeller_deice = 0, 5, 17
light_recognition = 0, 5, 17
light_wing = 0, 5, 17
light_logo = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 0, 17
directional_gyro_slaving = 0, 0, 17

[flight_tuning]
cruise_lift_scalar=0.8 
parasite_drag_scalar=0.7 
induced_drag_scalar=1.1 
elevator_effectiveness=0.8 
aileron_effectiveness=0.9 
rudder_effectiveness=1.0 
pitch_stability=1.2 
roll_stability=1.2 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=0.8 
rudder_trim_effectiveness=0.8 

[propeller]
thrust_scalar=1.1 
propeller_type=0 
propeller_diameter=12.2 
propeller_blades=6 
propeller_moi=76 
beta_max=50.0 
beta_min=3 
min_gov_rpm=12000 
prop_tc=0.1 
gear_reduction_ratio=12.5 
fixed_pitch_beta=0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=600 
beta_feather=82.0 
power_absorbed_cf=0.9 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0 
minimum_reverse_beta=-18.5 
feathering_switches=1 

[TurbineEngineData]
fuel_flow_gain=0.012 // 0.040
inlet_area=1 
rated_N2_rpm=15000.000 //13750.000 
static_thrust=198.000 

[turboprop_engine]
maximum_torque=10794.00 //12091.00 
power_scalar=1.000 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
afterburner_available=1 

[gear_warning_system]
gear_warning_available=0    
pct_throttle_limit=0    
flap_limit_idle=0       
flap_limit_power=0      
[brakes]
parking_brake = 1       
toe_brakes_scale = 0.6  
differential_braking_scale =0.5
auto_brakes = 0
[hydraulic_system]
electric_pumps=1
engine_map=1,0,0,0
normal_pressure=2090.8310000
  
                               
[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1, 1 
Adf.2=1, 1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=4,2 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15   
vacuum_type=2
       
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    

[Reference Speeds]
flaps_up_stall_speed=50.000   //70
full_flaps_stall_speed=45.000 
cruise_speed=120.000 
max_indicated_speed=242.000000
max_mach=0.60000

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0.0 
default_bank_mode=0
default_pitch_mode=0
autothrottle_available=0 
pitch_takeoff_ga=8.0 
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=2
     
[exits]
number_of_exits = 1
exit.0 = 0.4 // (0=Main 1=Emergency)

[Flaps.0]
type= 1
span-outboard= 0.600
extending-time= 30.000
system_type= 1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.300   //1.300
drag_scalar= 1.600  
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000

