[fltsim.0]
title=Ilyushin Il-18 LOT 70
sim=Il18-V7-0
model=
panel=
sound=
texture=LOT70
kb_checklists=
kb_reference=
atc_id=SP-LSF
atc_airline=LOT
atc_flight_number=754
ui_manufacturer=Ilyushin
ui_type=IL-18
ui_variation=LOT Mid 70s
editable=1
description=The Ilyushin Il-18 (NATO reporting name: Coot) is a large turboprop airliner that became one of the best known Soviet aircraft of its era as well as one of the most popular and durable, having first flown in 1957 and still in use over 50 years later. The Il-18 was one of the world's principal airliners for several decades and was widely exported. Due to the aircraft's airframe durability, many achieved over 45,000 flight hours. The Il-18's successor was the long range Il-62 jet airl
atc_heavy=0
prop_anim_ratio=1.7

[fltsim.1]
title=Ilyushin Il-18 LOT 80
sim=Il18-V7-0
model=
panel=
sound=
texture=LOT80
kb_checklists=
kb_reference=
atc_id=SP-LSD
atc_airline=LOT
atc_flight_number=7541
ui_manufacturer=Ilyushin
ui_type=IL-18
ui_variation=LOT Mid 80s
editable=1
description=The Ilyushin Il-18 (NATO reporting name: Coot) is a large turboprop airliner that became one of the best known Soviet aircraft of its era as well as one of the most popular and durable, having first flown in 1957 and still in use over 50 years later. The Il-18 was one of the world's principal airliners for several decades and was widely exported. Due to the aircraft's airframe durability, many achieved over 45,000 flight hours. The Il-18's successor was the long range Il-62 jet airl 
atc_heavy=0
prop_anim_ratio=1.7

[fltsim.2]
title=Ilyushin Il-18 Aeroflot
sim=Il18-V7-0
model=
panel=
sound=
texture=75478
kb_checklists=
kb_reference=
atc_id=RA-75478
atc_airline=Aeroflot
atc_flight_number=75478
ui_manufacturer=Ilyushin
ui_type=IL-18
ui_variation=Aeroflot
editable=1
description=The Ilyushin Il-18 (NATO reporting name: Coot) is a large turboprop airliner that became one of the best known Soviet aircraft of its era as well as one of the most popular and durable, having first flown in 1957 and still in use over 50 years later. The Il-18 was one of the world's principal airliners for several decades and was widely exported. Due to the aircraft's airframe durability, many achieved over 45,000 flight hours. The Il-18's successor was the long range Il-62 jet airl  
atc_heavy=0
prop_anim_ratio=1.7

[General]
performance=Four-Engine Long-range Turboprop Airliner\nFour-Engine Turboprop\n\n  - FD by AAV -V7.0
atc_type=
atc_model=IL-18
Category=airplane


[weight_and_balance]
empty_weight=78202//[35.5t]
max_gross_weight=141000//[64t]   

reference_datum_position=0, 0, 0
empty_weight_cg_position=1.784, 0.000, 0.160
empty_weight_pitch_MOI=2500000.
empty_weight_roll_MOI=2700000.
empty_weight_yaw_MOI=2500000. 
empty_weight_coupled_MOI=0

max_number_of_stations=10
station_load.0=3395., 20.000, 0.000,  1.0, Front 
station_load.1=5247., -8.000, 0.000,  1.0, Center 
station_load.2=1080., -30.00, 0.000,  1.0, Rear 
station_load.3=1865., 15.000, 0.000, -0.33, Front_Cargo 
station_load.4=807., -20.500, 0.000, -0.33, Rear_Cargo 
//

[GeneralEngineData]
engine_type=5
Engine.0=12.792, -29.848, -1.
Engine.1=15.416, -14.760, -1.
Engine.2=15.416, 14.760,  -1.
Engine.3=12.792, 29.848,  -1.
//
fuel_flow_scalar=0.75
min_throttle_limit=-0.001
max_contrail_temperature=-35


[TurbineEngineData]
fuel_flow_gain=0.01//aav//0.005 
inlet_area=1.5 
rated_N2_rpm=27920 
static_thrust=500. 
afterburner_available=0
reverser_available=0.0

[turboprop_engine]
power_scalar  = 1.0 
maximum_torque= 13700.   

[propeller]
thrust_scalar=1.0                  //Propeller thrust scalar
propeller_type=0                  //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12             //Propeller Diameter, (feet)
propeller_blades=4                //Number of propeller blades
propeller_moi=100.                 //Propeller moment of inertia
beta_max=50.                      //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=8.//10.0                 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25500                 //Miminum governed RPM
prop_tc=0.01                      //Prop time-constant
gear_reduction_ratio=15.4         //Propeller gear reduction ratio
fixed_pitch_beta=0                //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=55.        //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1             //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1            //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1       //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1   //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=500.           //Minimum RPM for prop feathering
beta_feather=93.                   //Feathering pitch angle (degrees)
power_absorbed_cf=0.95             //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0  //Defeathering accumulators available? 0=FALSE,1=TRUE
prop_reverse_available=1.0             //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0            //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=1                 //Minimum pitch angle in reverse, (degrees)
rotation=-1 -1 -1 -1                  //
//rotation=1 1 1 1                  //



[FLIGHT_TUNING]
cruise_lift_scalar  =1.0 
parasite_drag_scalar=0.9
induced_drag_scalar =1.5
elevator_effectiveness= 1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=1.5 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00
//
//p_factor_on_yaw=-1.0
//torgue_on_roll=-1.0
//gyro_precession_on_roll=-1.0
//gyro_precession_on_yaw=-1.0


[electrical]
max_battery_voltage=24.0
generator_alternator_voltate=28.0
max_generator_alternator_amps=600.0
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17
avionics=1, 5 , 17
pitot_heat=0, 15, 17.0
additional_system=0, 2 , 10
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17
starter1=0, 20, 160
starter2=0, 20, 160
starter3=0, 20, 160
starter4=0, 20, 160
light_nav=0, 5 , 4
light_beacon=0, 10 , 4
light_landing=0, 15 , 12
light_taxi=0, 10 , 4
light_strobe=0, 5 , 6
light_panel=0, 5 , 2


[fuel]
//
// 6.7 lbs/gal; -> 3.04liters/Gal -> (1Gal=3.786liters) -> Ro~0.8
//
/  [ 1t ~ 330.164 Gal ] 
//
//  Total   ~23.55t
// Tank # 12
Center1  =-0.540, 0.0,     0.0,   1113.233, 0.0   // Tank #12; max: 4950kg 
	// Left wing
External1= 0.309, -19.193, 2.950, 264.172, 0.000  // Raskhodnyi Bak (#1, #3); max:800kg 
LeftAux = 0.656, -24.606, 2.950, 1271.411, 0.000	  // I group of tanks (#2, #4 to #7); 
LeftTip = 0.140, -50.200, 3.100, 855.257, 0.000	  // Tank # 8 (0 group); max:2590kg 
Center2 = 0.322, -10.390, 1.960, 944.416, 0.000	  // II  group of tanks (#9 to #11); max:2860kg 
// Right wing
External2= 0.309, 19.193, 2.950, 264.172, 0.000  // Raskhodnyi Bak (#1, #3) 
RightAux = 0.656, 24.606, 2.950, 1271.411,0.000	  // I group of tanks (#2, #4 to #7) 
RightTip = 0.140, 50.200, 3.100, 855.257, 0.000	  // Tank # 8 (0 group) 
Center3  = 0.322, 10.390, 1.960, 944.416, 0.000	  // II  group of tanks (#9 to #11) 
//
fuel_type=2.0
number_of_tank_selectors=4
electric_pump=1


//==============================================================
//===================GEOMETRY===================================
//==============================================================

[airplane_geometry]
wing_area      = 1340 
wing_span      = 122. 
wing_root_chord= 11.  
wing_dihedral  = 0.0
wing_incidence = 0 
wing_twist=0
wing_winglets_flag = 0
wing_sweep         = 0.0
wing_pos_apex_lon  = 3.6//2.7//3.5
wing_pos_apex_vert = 2 
oswald_efficiency_factor=0.8 
//
htail_area=250.
htail_span=34.
htail_pos_lon=-52.//-63.0 
htail_pos_vert=3.5 
htail_incidence=0.
htail_sweep= 10.
//
vtail_area=200.
vtail_span=18.0
vtail_sweep=25.0 
vtail_pos_lon=-46//-57.
vtail_pos_vert=8.0 
//
elevator_area=70.0 
aileron_area =50.0 
rudder_area  =65. 
elevator_up_limit=28
elevator_down_limit=15
aileron_up_limit=25
aileron_down_limit=15
rudder_limit= 25.0 
elevator_trim_limit=12
//spoiler_limit=0.
//
spoiler_limit=1
spoiler_handle_available=1
//
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0
spoilerons_available=0
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000


[contact_points]
//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//1  Longitudinal Position        (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Damage Threshold      (Feet Per Minute)
//5  Brake Map                    (0=None, 1=Left, 2=Right)
//6  Wheel Radius                 (feet)
//7  Steer Angle                  (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio                (0=Undamped, 1=Critically damped)
//11 Extension Time               (seconds)
//12 Retraction Time              (seconds)
//13 Sound Type
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
  
//wheels
point.0=1.000, 42.305, 0.000, -9.150, 1200.000, 0.000, 1.148, 85.000, 0.300, 2.000, 0.85, 14.000, 15.000, 0.000, 219.000, 232.000  //center gear
point.1=1.000, -1.548, -14.760,-9.150,  1600.000, 1.000, 1.476, 0.000, 0.400, 2.000, 0.85, 14.000, 15.000, 2.000, 219.000, 232.000  //left gear
point.2=1.000, -1.548, 14.760, -9.150,  1600.000, 2.000, 1.476, 0.000, 0.400, 2.000, 0.85, 14.000, 15.000, 3.000, 219.000, 232.000  //right gear
//right gear
//point.0=1.000, 40.305, 0.000, -8.650, 1200.000, 0.000, 1.148, 32.000, 0.300, 2.000, 0.500, 10.000, 12.000, 0.000, 219.000, 232.000  //center gear
//point.1=1.000, -1.548, -14.760, -8.950, 1600.000, 1.000, 1.476, 0.000, 0.400, 2.000, 0.900, 14.000, 15.000, 2.000, 219.000, 232.000  //left gear
//point.2=1.000, -1.548, 14.760, -8.950, 1600.000, 2.000, 1.476, 0.000, 0.400, 2.000, 0.900, 12.000, 14.000, 3.000, 219.000, 232.000  //right gear
//point.0=1.000, 40.305, 0.000, -8.650, 1200.000, 0.000, 1.148, 32.000, 0.300, 2.000, 0.500, 10.000, 12.000, 0.000, 219.000, 232.000  //center gear
//point.1=1.000, -1.548, -14.760, -8.950, 1600.000, 1.000, 1.476, 0.000, 0.400, 2.000, 0.900, 14.000, 15.000, 2.000, 219.000, 232.000  //left gear
//point.2=1.000, -1.548, 14.760, -8.950, 1600.000, 2.000, 1.476, 0.000, 0.400, 2.000, 0.900, 12.000, 14.000, 3.000, 219.000, 232.000  //right gear
  //scrape
point.3=2.000, 53.900, 0.000, 0.000,  400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000     //nose
point.4=2.000, -63.00, 0.000, 4.500, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //tail
point.5=2.000, 0.000, -61.300, 1.600, 600.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000     //left wing tip
point.6=2.000, 0.000, 61.300, 1.600, 600.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //right wing tip

point.7=2.000, -58.000, -19.400, 3.600, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //ht left tip
point.8=2.000, -58.000, 19.400, 3.600, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //ht right tip
point.9=2.000, -58.000, 0.000, 25.300, 500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //vt 1

point.10=2.000, -25.000, 0.000, 7.800, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //upper line 1
point.11=2.000,  29.000, 0.000, 7.000, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //upper line 2

point.12=2.000, 37.000, 0.000, -4.500,  400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //bottom line 1
point.13=2.000, -18.500, 0.000, -2.800, 400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //bottom line 2
point.14=2.000, -45.600, 0.000, -2.000, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000     //fuse

//
max_number_of_points=14
static_pitch=0
static_cg_height=8.530
gear_system_type=0




[Reference Speeds]
flaps_up_stall_speed=100.000
full_flaps_stall_speed=83.800
cruise_speed=310.000
max_indicated_speed=330.000000
max_mach=0.650000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=42.056,-1.716, 4.500
//eyepoint=31.056,-1.716, 4.500

[autopilot]
autopilot_available=1 //!!!! AAV
flight_director_available=1
default_vertical_speed=100.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=110
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
autoland_available=0
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=5.
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.5
max_pitch_velocity_lo_alt_breakpoint=16000.
max_pitch_velocity_hi_alt_breakpoint=20000.0
max_bank=15.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000

//OLD
//autopilot_available=0
//flight_director_available=0
//default_vertical_speed=100.0
//autothrottle_available=0
//autothrottle_arming_required=0
//autothrottle_takeoff_ga=100
//autothrottle_max_rpm=90.000000
//pitch_takeoff_ga=9.000000
////For no wing leveler when AP On
//use_no_default_bank=1
////For no pitch holding when AP On
//use_no_default_pitch=1
////Nothing autoland, only hand
//autoland_available=0

[direction_indicators]
direction_indicator.0=2,0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1,0
Adf.2=1,0
Transponder.1=1
Marker.1=1

[pitot_static]
vertical_speed_time_constant=10                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_154, 1
startup=il 18_engstart.fx, 1


//=====================================================   
///================FLAPS==============================   
///=====================================================   

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 220.000
blowout-speed= 250.000
lift_scalar= 0.0
drag_scalar= 0.0 
pitch_scalar= 1.000
flaps-position.0= 0.000,  0.000
flaps-position.1= 5.000,  200.0
flaps-position.2= 10.000, 200.0
flaps-position.3= 15.000, 180.0
flaps-position.4= 30.000, 165.0
//
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 270.000
blowout-speed= 320.000
lift_scalar= 1.0 
drag_scalar= 0.0 
pitch_scalar= 0.000
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= 32.000, 0.000
//
[Flaps.2]
type= 1
span-outboard= 0.800
extending-time= 20.
system_type= 0
damaging-speed= 270.000
blowout-speed= 320.000
lift_scalar= 0.0 
drag_scalar= 1.0  
pitch_scalar= 0.000
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= 35.000, 0.000



[LIGHTS]
/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//-------НАВИГАЦИОННЫЕ-------
//левое крыло, передний
light.0=3, 1.3, -62.3, 1.8, fx_navredh,
//правое крыло передний
light.1=3, 1.3, 62.3, 1.8, fx_navgreh,
//левое крыло, задний
light.2=3, -0.5, -62.3, 1.8, fx_navredh,
//правое крыло, задний
light.3=3, -0.5, 62.3, 1.8, fx_navgrem,
//

light.4  = 4, 68.0, 0.0, 25.90, fx_vclight_154vH ,
light.5  = 1, -43.3, 0.00, -2.42,  fx_vclight,
light.6  = 4, 41.0, -0.15, 0.56, fx_vclighth ,
light.7  = 4, 10.0, -1.10, 7.00, fx_vclighth ,--
light.8  = 4, -25.0, -1.10, 7.00, fx_vclighth ,
light.9  = 5, 2.5, 60.50, 0.80,fx_Shockwave_landing_light_narrow , 
light.10 = 5, 2.5, -60.50, 0.80,fx_Shockwave_landing_light_narrow ,  
light.11 = 5, 59.3, -3.30, -2.1, fx_ES_3d-lights_VC_blue // ES 3D Lights (2D and VC landing light)
light.12 = 5, 59.3, 3.30, -2.1, fx_ES_3d-lights_VC_blue // ES 3D Lights (2D and VC landing light)
light.13 = 5, 45.50, 4.20, -2.30,fx_Shockwave_landing_light_narrow , 
light.14 = 5, 45.50, -4.20, -2.30,fx_Shockwave_landing_light_narrow 

//-----Маяки-----
//нижний маяк (красный)
light.15=1, -39.0, 0.00, -2.60, fx_beaconb
//верхний маяк (красный)
light.16=1, -57.5, 0.00, 26.25, fx_beaconb

[smokesystem]
smoke.0=0.000, -15.00, -30.00, fx_nicksmoke747 
smoke.1=-1.000, -17.00, -14.80, fx_nicksmoke747
smoke.2=-1.000, -17.00, 14.80, fx_nicksmoke747
smoke.3=0.000, -15.00, 30.00, fx_nicksmoke747

[brakes]
toe_brakes_scale=0.4
parking_brake=1.0
differential_braking_scale= 1.0
auto_brakes=4

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
gear_bump_nose_magnitude=3000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=2700		; 0 - 10000
gear_bump_left_direction=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=1300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000			; 0 - 10000
crash_direction1=01000			; 0 - 35999 degrees
crash_magnitude2=10000			; 0 - 10000
crash_direction2=9000			; 0 - 35999 degrees
crash_period2=75000			; in microseconds
crash_duration2=2500000			; in microseconds
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2