[fltsim.0]
title=MI-17 Transport
sim=MI17
model=
panel=
sound=
texture=m
kb_checklists=
kb_reference=
prop_anim_ratio=-1.75
atc_id_color=
atc_id=87
atc_model=
ui_manufacturer=Kazan Helicopter Plant JSC
ui_type=Mi-17-1V
ui_variation=Armed Forces of Ukraine No.81
description=Hitory:\nThe first version ( V-8 ) flew in 1961 and constructed by Mikhail Leontievich Mil (1909-1970), father of the Mil Helicopter Plant. In 1962 the Izotov TV2-117 shaft-turbine engine, in 1963 a five blade main rotor system was installed in the aircraft. The serial production of Mi-8 (NATO code HIP) started in 1965. The MI-17 is an upgrade, equipped with stronger Izotov TV3-117 engine, vibration damper, lightweight fuselage, improved electronics and avionics. The production started in 1981. In 1988 the new TV3-117VM engine was build in ( MI-8MTV ).\n\nThe designation MI-17 is used in export, the russian army use the MI-8MTV marking. The MI-17 can be differentiate from MI-8 because the tail rotor is at the starboard side and the TV3-117 engine is shorter than theTV2-117. The helicopter can be used several purposes:\ncargo and troop transport, can be equipped with missiles, bombs, small arms and cannons. It can be modified to carry woundeds and medical corps. \n      \n
atc_heavy=0
atc_airline=Armed Forces of Ukraine
atc_flight_number=87

[fltsim.1]
title=MI-17 Parachute
sim=MI17
model=para
panel=
sound=
texture=para
kb_checklists=
kb_reference=
prop_anim_ratio=-1.75
atc_id_color=
atc_id=25754
atc_model=
ui_manufacturer=Kazan Helicopter Plant JSC
ui_type=Mi-17-1V
ui_variation=KAZAN (Parachute)
description=Hitory:\nThe first version ( V-8 ) flew in 1961 and constructed by Mikhail Leontievich Mil (1909-1970), father of the Mil Helicopter Plant. In 1962 the Izotov TV2-117 shaft-turbine engine, in 1963 a five blade main rotor system was installed in the aircraft. The serial production of Mi-8 (NATO code HIP) started in 1965. The MI-17 is an upgrade, equipped with stronger Izotov TV3-117 engine, vibration damper, lightweight fuselage, improved electronics and avionics. The production started in 1981. In 1988 the new TV3-117VM engine was build in ( MI-8MTV ).\n\nThe designation MI-17 is used in export, the russian army use the MI-8MTV marking. The MI-17 can be differentiate from MI-8 because the tail rotor is at the starboard side and the TV3-117 engine is shorter than theTV2-117. The helicopter can be used several purposes:\ncargo and troop transport, can be equipped with missiles, bombs, small arms and cannons. It can be modified to carry woundeds and medical corps. \n      \n
atc_heavy=0
atc_airline=Kazan
atc_flight_number=25754

[General]
atc_type=HELICOPTER
performance=Data:\nLenght (rotors turning): 25,4 m ( 83,3 ft )\nLenght (fuselage): 18,4 m ( 60,3 ft )\nHeight: 5,7 m ( 18,7 ft ) \nWitdth: 2,5 m ( 8,8 ft )\nMain rotor diameter: 21,3 m \/ 5 \/ ( 69,9 ft )\nTail Rotor diameter: 3,9 m \/ 3 \/ ( 12,8 ft )\nWeight: - Max gross: 13.000 kg ( 28668 lb ), Normal takeoff: 11.000 kg ( 24250 lb ), Emty:7.088-7.370 kg ( es. 15700 lb ) \nEngine: 2x1637 KW ( 2200 shp ) TV3-117VM turboshaft\nFuel: - Consumotion: 445 l ( 117 gal ) Port: 745 l ( 197 gal) Starboard: 680 l ( 749 gal )\nSpeed: - Maximum: 250 km\/h ( 135 knots ), Cruising: 240 km\/h ( 129 knots ) Ceiling: - Service: 5000-5700 m ( 16400-18700), Hover ( out of grnd effect ): 1760 m ( 5770 ), Hover ( in grnd effect ): 1900-3900 ( 6230- 12800 )\nClimb rate: 9 m\/s ( 30 ft\/s )\nPayload: - Internal: 4000 kg ( 8800 lb) External: 3000 kg ( 6600 lb )\n\n   \n 
atc_model=MI 17
Category=helicopter

[WEIGHT_AND_BALANCE]
max_gross_weight = 26000.000
empty_weight = 15553.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 7.709, 0.000, 0.000

max_number_of_stations = 50

station_load.0 =170.000000, 21.489000, -2.132000, -2.132000, Pilot
station_load.1 =170.000000, 21.489000, 2.135000, -2.132000, Co-Pilot
station_load.2 =170.000000, 20.177000, 0.000000, -2.130000, Engineer
station_load.3 =170.000000, 14.271000, -1.640000, -2.788000, Pass FrontLeft1
station_load.4 =170.000000, 14.271000, -3.280000, -2.788000, Pass FrontLeft2
station_load.5 =170.000000, 11.318000, -1.640000, -2.952000, Pass FRontLeft3
station_load.6 =170.000000, 11.318000, -3.280000, -2.952000, Pass FrontLeft4
station_load.7 =170.000000, 8.202000, -1.640000, -3.280000, Pass MiddleLeft
station_load.8 =170.000000, 8.202000, -3.280000, -3.280000, Pass MiddleLeft
station_load.9 =170.000000, 5.249000, -1.640000, -3.444000, Pass BackLeft1
station_load.10 =170.000000, 5.249000, -3.280000, -3.444000, Pass BackLeft2
station_load.11 =170.000000, 2.600000, -1.640000, -3.608000, Pass BackLeft3
station_load.12 =170.000000, 2.600000, -3.280000, -3.608000, Pass BackLeft4
station_load.13 =170.000000, 14.271000, 1.640000, -2.788000, Pass FrontRight
station_load.14 =170.000000, 14.271000, 3.280000, -2.788000, Pass FrontRight
station_load.15 =170.000000, 11.318000, 1.640000, -2.952000, Pass FRontRight
station_load.16 =170.000000, 11.318000, 3.280000, -2.952000, Pass FrontRight
station_load.17 =170.000000, 8.202000, 1.640000, -3.280000, Pass MiddleRigh
station_load.18 =170.000000, 8.202000, 3.280000, -3.280000, Pass MiddleRigh
station_load.19 =170.000000, 5.249000, 1.640000, -3.444000, Pass BackRight1
station_load.20 =170.000000, 5.249000, 3.280000, -3.444000, Pass BackRight2
station_load.21 =170.000000, 2.600000, 1.640000, -3.608000, Pass BackRight3
station_load.22 =170.000000, 2.600000, 3.280000, -3.608000, Pass BackRight4

;Moments of Inertia
empty_weight_roll_MOI= 50000.000
empty_weight_pitch_MOI= 50000.000
empty_weight_yaw_MOI= 106000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
rudder_effectiveness=0.05
aileron_effectiveness= 1.0
elevator_effectiveness=1.3

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 4, 4 , 15.0
avionics           = 0, 5 , 15.0
pitot_heat         = 4, 2 , 15.0
additional_system  = 0, 2 , 15.0
marker_beacon      = 4, 2 , 10.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 24.0
starter2           = 0, 20, 24.0
starter3           = 0, 20, 24.0
light_nav          = 0, 5 , 10.0
light_beacon       = 4, 5 , 15.0
light_landing      = 4, 5 , 15.0
light_taxi         = 0, 5 , 15.0
light_strobe       = 0, 5 , 10.0
light_panel        = 0, 5 , 10.0
light_cabin        = 4, 5 , 10.0
light_logo         = 4, 5 , 10.0
light_recognition  = 4, 5 , 10.0
hydraulic_pump     = 0, 5 , 15.0
fuel_transfer_pump = 0, 5 , 15.0
max_battery_voltage = 38.0
generator_alternator_voltage = 208.0
max_generator_alternator_amps = 150.0


        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //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)

[contact_points]
point.0= 1.000, 18.864, 0.000, -8.850, 1574.000, 0.000, 0.984, 35.000, 0.760, 1.300, 0.750, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 4.757, -7.381, -8.700, 1600.000, 1.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 4.757, 7.381, -8.700, 1600.000, 2.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 25.754, 0.000, -4.101, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.4= 2.000, -2.460, 0.000, -6.233, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 8.366
point.5= 2.000, -27.887, 0.000, -4.800, 600.000, 0.000, 0.000, 0.000, 0.600, 1.500, 0.850, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 42.800, 0.000, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.7= 2.000, -27.060, 0.000, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000
point.8= 2.000, -7.830, -34.930, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.9= 2.000, -7.830, 34.930, 6.560, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.10= 2.000, -32.800, -0.820, -2.460, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000
point.11= 2.000, -39.360, -0.820, 3.930, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000

[brakes]
parking_brake = 1      //Parking brake available
toe_brakes_scale = 0.3  //Brake scalar
auto_brakes=4

[hydraulic_system]
normal_pressure=797.700
engine_map=1,0,0,0
electric_pumps=1

[Views]
eyepoint = 20.4, -2.15, -0.25

[exits]
number_of_exits=4
exit_rate.0=0.4                                                           
exit_rate.1=0.4      
exit_rate.2=0.4
exit_rate.3=0.4

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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[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=2,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 23.23, -3.58, -3.29,  fx_navred ,
light.1 = 3, 23.23, 3.58, -3.29,  fx_navgre ,
light.2 = 3, -32.48,  0.00, -0.07,  fx_navwhi ,
light.3 = 1, -14.10,  0.10, 2.00,  fx_beacon ,
light.4 = 2, 23.23,  -3.58, -3.29,  fx_strobe ,
light.5 = 4, 22.47,  -2.00, 0.00,  fx_vclight ,
light.6 = 4, 22.47,  2.00, 0.00, fx_vclight ,
light.7 = 5, 23.00, 0.50, -5.00, fx_landing ,
light.8 = 5, 23.00, -0.50, -5.00, fx_landing ,
light.9 = 2, 23.23,  3.58, -3.29,  fx_strobe ,
light.10 = 2, -32.48,  0.00, -0.07,  fx_strobe ,
light.11 = 6, 19.50, -0.50, -6.30, fx_landing ,
light.12 = 10, 15.00,  0.00, -2.50, fx_vclighth ,
light.13 = 10, 6.00,  0.00, -3.00, fx_vclighth ,
light.14 = 9, -34.50,  0.00, 5.30, fx_recog ,

//=================================================
[SMOKESYSTEM]
smoke.0=-20.00, 0.00, -5.42, ZH_ikpp.fx     /// 1 click-5 second!

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt
landrotorwas=fx_rtr_lnd
waterrotorwash=fx_rtr_wt
touchdown=fx_tchdwn
deice=fx_deicing

[fuel]
Center1 = 6.889, 0.000, 2.296, 117.000, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =3                    
electric_pump=1
External1= 8.366, -4.920, -4.757, 179.000, 0.000
External2= 9.350, 4.920, -4.757, 196.000, 0.000

[GeneralEngineData]
engine_type = 1
Engine.0 = 11.975, -0.984, 2.624
Engine.1 = 11.975, 0.984, 2.624
Engine.2 = 5.000, 0.000, 3.000
fuel_flow_scalar = 5.100
min_throttle_limit =  0.0;                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -60.0
master_ignition_switch = 1

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 4.772
rated_N2_rpm= 15000.000
static_thrust= 2225.000
afterburner_available= 0
reverser_available= 0.000

[Reference Speeds]
cruise_speed            = 129.0                 //Knots True (KTAS)
max_indicated_speed     = 134.0                   //Red line (KIAS)

[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=1.500000
roll_damp_cf=1.000000
yaw_damp_cf=0.600000
yaw_stability_cf=2.500000

[MainRotor]
Position = 7.873, 0, 6.561
Radius = 34.931
max_disc_angle = 4.0
Number_of_blades = 5
weight_per_blade = 264.0
Weight_to_moi_factor = 42.0
inflow_wel_reference =43.0
inflow_vel_reference=0.000000
 
[SecondaryRotor]
TailRotor = 1
Position = -34.776, 2.378, 4.101
Radius = 6.397 

[autopilot]
autopilot_available= 1
flight_director_available= 0
attitude_indicator= 0
direction_indicator=0
default_pitch_mode=1
max_pitch=20.0
max_pitch_acceleration=5.0
default_vertical_speed=0.01
default_bank_mode=2
max_bank=30
max_bank_acceleration=1.5
autothrottle_available=0
pitch_takeoff_ga= 8.000
max_pitch_velocity_lo_alt= 5.000
max_pitch_velocity_hi_alt= 5.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank_velocity= 5.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 5.000

[yaw_string]
yaw_string_available=1

[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=5.150000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
[CameraDefinition.201]
Title=EZdok Aircraft Universal camera
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC65B}
Description=Universal camera for EZdok cam utility
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.40
ShowWeather=Yes
InitialXyz=0,0,0
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
HotKeySelect=4
