[fltsim.0]
title=Mi-171
sim=Mi-171
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=-1.05
atc_id=OM-AVO
atc_model=Mi-171
ui_manufacturer=Mil Helicopters
ui_type=Mi-171
ui_variation=OM-AVO
atc_heavy=0
atc_airline=UTAIR
atc_flight_number=OM-AVO
[General]
Mi-171
Crew: Three – two pilots and one engineer,Capacity: 30 troops or 12 stretchers or 4,000 kg ,Length: 18.465 m,Empty weight: 7,489 kg,
Loaded weight: 11,100 kg,powered by two Klimov TV3-117VM turboshaft engines.
[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, -8.650, 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, -8.560, 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, -8.560, 1600.000, 2.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 3.000, 0.000, 0.000
static_pitch = 3.8
static_cg_height = 8.366
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.3 //Brake scalar
[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,5=landing
light.1 = 1, -8.600, -0.100, 2.00, fx_beacon ,
light.2 = 1, 22.900, -1.100, -5.10, fx_beacon
light.3 = 5, 26.00, 0.40, -4.60, fx_landing ,
light.5 = 5, 26.00, -0.40, -4.60, fx_landing ,
[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