[fltsim.0]
title=Project Tupolev IL-62M_V1_03
sim=Il-62M_V0_034
panel=
model=
sound=
texture=
checklists=
ui_manufacturer=Ilyushin
ui_type=PT_IL-62M
ui_variation=Aeroflot AIRLINES
description=IL-62M model version 1.03
atc_heavy=0
atc_id=86520
atc_airline=Aeroflot Airlines
atc_flight_number=86520
atc_id_color=0000000000
visual_damage=0

[weight_and_balance]

max_gross_weight = 364000.0
//empty_weight = 149118.78
empty_weight = 149000.0
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.0, 0, 0
empty_weight_pitch_MOI = 5761006
empty_weight_roll_MOI = 1624758
empty_weight_yaw_MOI = 4946572
empty_weight_coupled_MOI = 400
max_number_of_stations = 3

station_load.0 = 9000.6,-48.484,0.0,0.0
station_load.1 = 15000,69,0.0,0.0
station_load.2 = 15000.4,-49,0.0,0.0


[lights]

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

light.0 = 3, -31.9, -70.0,  -0.6, fx_navredm ,
light.1 = 3, -31.9, 70.0,  -0.6, fx_navgrem ,
light.2 = 3, -71.10,   0.60,  4.00, fx_navwhih ,
light.3 = 2,   24.0,   0.40, -5.72, fx_beaconb ,
light.4 = 1,   -75.70,   0.60,  27.80, fx_beaconh ,
light.5 = 4,  79.9,   0.90,  5.10, fx_vclight ,
light.6 = 5,  80.5, -4.33, -2.0, fx_landing.fx ,
light.7 = 5,  80.5, 3.7, -3.7, fx_landing.fx ,
light.8 = 5,  -10.4, -39.1, -2.47, fx_landing.fx ,
light.9 = 3, -10.4, 39.1, -2.47, fx_landing.fx

[smokesystem]
smoke.0 = -1.3,-56.1,-16.8, fx_smoke_rx
smoke.1 = -1.3,-56.1,-10.20, fx_smoke_rx
smoke.2 = -1.3,-56.1,10.20, fx_smoke_rx
smoke.3 = -1.3,-56.1,16.8, fx_smoke_rx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_154, 1

[fuel]
Center1   =  0.0,   0.0, -4.0, 13130.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -7.0, -35.0,  0.0, 6565.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -7.0,  35.0,  0.0, 6565.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 4

//1

electric_pump=0


        //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)

[contact_points]
static_pitch = 0
static_cg_height = 11.3
max_number_of_points = 5
//          0       1       2        3        4          5       6       7       8     9      10    11      12      13     14       15
point.0 = 1.000, 72.200,  0.000,  -12.100,  900.000,  0.000,  1.500, 55.000, 0.656, 2.000, 0.550, 10.000, 10.000, 0.000, 300.000, 300.000
point.1 = 1.000, -6.6,  -12.500, -11.900,  1100.000,  1.000,  2.380,  0.000, 0.820, 2.000, 0.950, 12.800, 12.800, 2.000, 300.000, 300.000
point.2 = 1.000, -6.6,   12.500, -11.900,  1100.000,  2.000,  2.380,  0.000, 0.820, 2.000, 0.950, 12.800, 12.800, 3.000, 0.000, 0.000
point.3 = 5.000, -50.5,    0, -3.5, 0, 0, 0, 0, 0, 0, 0, 30, 30, 0, 0, 0
point.4 = 2.000, -50.500, 0.000, -3.500, 2000.000, 0.000, 1.000, 80.000, 0.600, 1.200, 0.98, 0.000, 0.000, 0.000, 300.000, 300.000
gear_system_type=0

//point.0 = 1.000, 72.200,  0.000,  -12.100,  800.000,  0.000,  1.500, 55.000, 0.600, 1.780, 0.550, 10.000, 10.000, 0.000, 300.000, 300.000
//point.1 = 1.000, -6.6,  -12.500, -11.900,   800.000,  1.000,  2.380,  0.000, 0.752, 1.050, 0.950, 12.800, 12.800, 2.000, 300.000, 300.000
//point.2 = 1.000, -6.6,   12.500, -11.900,   800.000,  2.000,  2.380,  0.000, 0.752, 1.050, 0.950, 12.800, 12.800, 3.000, 0.000, 0.000


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


[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000


[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type=1
fuel_flow_scalar=1.472
engine.0=-54.167, -15.583, 3.333
engine.1=-54.167, -11.000, 3.333
engine.2=-54.167, 11.000, 3.333
engine.3=-54.167, 15.583, 3.333
//min_throttle_limit=-0.169983
min_throttle_limit=-0.53

[airplane_geometry]
wing_area=3009.051
wing_span=141.73
wing_root_chord=24.8
wing_dihedral=3.183
wing_incidence=3.000
wing_twist=-4
oswald_efficiency_factor=0.9
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=6.200
wing_pos_apex_vert=0.000
htail_area=430.55
htail_span=40.13
htail_pos_lon=-73.167
htail_pos_vert=0.000
htail_incidence=-3.00
htail_sweep=0.000
vtail_area=383.19
vtail_span=25.59
vtail_sweep=0.000
vtail_pos_lon=-70.833
vtail_pos_vert=21.667
elevator_area=87.73
aileron_area=87.435
rudder_area=101.83
elevator_up_limit=26
elevator_down_limit=15
aileron_up_limit=27
aileron_down_limit=16
rudder_limit=27
//elevator_trim_limit=10
elevator_trim_limit=6.0
//spoiler_limit=60
spoiler_limit=45
aileron_to_spoileron_gain=2.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
//spoilerons_available=1
spoilerons_available=0

//;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)


[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0

flap_motor         = 0, 0.05 , 17.0
gear_motor         = 0, 0.05 , 17.0
autopilot          = 0, 0.05 , 17.0
avionics_bus       = 0, 0.05,  17.0
avionics           = 0, 0.05 , 17.0
pitot_heat         = 0, 0.05 , 17.0
additional_system  = 0, 0.05,  17.0
marker_beacon      = 0, 0.05 , 17.0
gear_warning       = 0, 0.05 , 17.0
fuel_pump          = 0, 0.05 , 17.0
starter1           = 0, 0.05 , 17.0
light_nav          = 0, 0.05 , 17.0
light_beacon       = 0, 0.05 , 17.0
light_landing      = 0, 0.05 , 17.0
light_taxi         = 0, 0.05 , 17.0
light_strobe       = 0, 0.05 , 17.0
light_panel        = 0, 0.05 , 17.0





[TurbineEngineData]
fuel_flow_gain=0.498
bypass_ratio=5.30
inlet_area=14.290
rated_N2_rpm=33000.000
static_thrust=24300.000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=180.000
full_flaps_stall_speed=110.000
cruise_speed=485.914
max_indicated_speed=571.000000
max_mach=0.9

[General]
performance=
atc_type=ILYUSHIN
atc_model=Il-62
editable=0
Category=airplane

[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, 1
Adf.1=1, 0
Adf.2=1, 0
Transponder.1=1
Marker.1=1

[direction_indicators]
direction_indicator.0=3,0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=110.000
pitch_takeoff_ga=8 ;
autoland_available=1
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=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
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

[Flaps.0]
type= 1
span-outboard= 0.620
extending-time= 20.000
system_type= 0
damaging-speed= 217.000
blowout-speed= 220.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 15.000, 0.000
flaps-position.2= 30.000, 0.000

[pitot_static]
//vertical_speed_time_constant=2
vertical_speed_time_constant=20

[exits]
number_of_exits=2
exit_rate.0=0.4
exit_rate.1=0.6

[direction_indicators]
direction_indicator.0=3,0

[Views]
eyepoint=70.34,-1.499446,7.04

[brakes]
toe_brakes_scale=0.5
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

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

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0