[General]
atc_type=ILYUSHIN 
atc_model=IL62 
editable=1 
performance= 
// FDE Template TwinEngineCommercialJetHeavy
// FDE Design   Jan Martin
// FDE Version  v5acofadv 

[Reference Speeds]
flaps_up_stall_speed=112.5 
full_flaps_stall_speed=112.5 
cruise_speed=590.0 
max_mach                = 0.99
max_indicated_speed     = 390.0

[weight_and_balance]
max_gross_weight = 364000
empty_weight = 149000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 10, 0, 0
empty_weight_pitch_MOI = 27500000
empty_weight_roll_MOI = 10000000
empty_weight_yaw_MOI = 16300000
empty_weight_coupled_MOI = 0
max_number_of_stations = 0
station_load.0 = 107500, 40, 0, 6
station_load.1 = 107500, -40, 0, 6


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -33.60,-70.90,  5.90, fx_navredh ,
light.1 = 3, -33.60, 70.90,  5.90, fx_navgreh ,
light.2 = 3, -74.00,  0.00, 11.50, fx_navwhih ,
light.3 = 1, -78.70,  0.00, 35.10, fx_beaconh ,
light.4 = 1,  21.00,  0.00,  0.50, fx_beaconb ,
light.5 = 2, -33.10, 70.85,  5.80, fx_strobeh ,
light.6 = 2, -33.10,-70.85,  5.80, fx_strobeh ,
light.7 = 2, -41.15, 70.50,  6.05, fx_strobeh ,
light.8 = 2, -41.15,-70.50,  6.05, fx_strobeh ,
light.9 = 2, -52, -16.7, 8.25, fx_tcai62smoke2 ,
light.10 = 2, -52, -10.7, 8.25, fx_tcai62smoke2 ,
light.11 = 2, -52, 10.7, 8.25, fx_tcai62smoke2 ,
light.12 = 2, -52, 17.2, 8.25, fx_tcai62smoke2 ,
light.13 = 1, -52, -16.7, 8.25, fx_tcai62smoke1 ,
light.14 = 1, -52, -10.7, 8.25, fx_tcai62smoke1 ,
light.15 = 1, -52, 10.7, 8.25, fx_tcai62smoke1 ,
light.16 = 1, -52, 17.2, 8.25, fx_tcai62smoke1

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.00
min_throttle_limit = -0.01
engine.0 = -52.5, -17.2, 8.5,
engine.1 = -52.5, -10.7, 8.5,
engine.2 = -52.5, 10.7, 8.5,
engine.3 = -52.5, 17.2, 8.5,

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tcai62tchdwn, 1
windshield_rain_effect_available = 1

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0
Center1 = 0, 0, -4, 26100, 3
LeftMain = -7, -35, 0, 9300, 3
RightMain = -7, 35, 0, 9300, 3


[contact_points]
static_pitch = -0.3
static_cg_height = 4.95
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 8
point.0 = 1, 67, 0, -5.68, 900, 0, 1.49, 110, 2.2, 0.5, 0.6, 10, 10, 0, 300, 300
point.1 = 1, -16, -11, -5.88, 1100, 1, 2.25, 0, 2.3, 0.75, 0.9, 12.8, 12.8, 2, 300, 300
point.2 = 1, -16, 11, -5.88, 1100, 2, 2.25, 0, 2.3, 0.75, 0.9, 12.8, 12.8, 3, 0, 0
point.3 = 2, -51.5, 0, 3, 2000, 0, 1, 80, 0.6, 2, 0.98, 0, 0, 9, 300, 300
point.4 = 2, -36.5, 70.5, 5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -36.5, -70.5, 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.6 = 2, -74, 0, 11.5, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.7 = 2, 87, 0, 6, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 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 = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
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

[airplane_geometry]
0,0,0,12.8016,2.3998,2.3998,1.4996,13.6611,4.7999,4.7999
2.9993,14.5207,7.1998,7.1998,4.4987,15.3802,9.5998,9.5998,5.9986,16.2399
11.9996,11.9996,7.4983,17.0995,14.3997,14.3997,8.9979,17.9589,16.7996,16.7996
10.4975,18.8185,19.1996,19.1996,11.9972,19.6781,21.5995,21.5995,13.4968,20.5377
0,0,0,7.1831,1.1971,1.1971,1.0045,7.8284,2.3942,2.3942
2.0090,8.4736,3.5915,3.5915,3.0136,9.1190,4.7887,4.7887,4.0180,9.7643
5.9857,5.9857,5.0226,10.4097,7.1831,7.1831,6.0272,11.0555,8.3802,8.3802
7.0317,11.7009,9.5774,9.5774,8.0361,12.3463,10.7746,10.7746,9.0410,12.9917
0,0,0,8.3210,0.9243,0.9243,0.6473,8.3027,1.8487,1.8487
1.2947,8.2840,2.7736,2.7736,1.9421,8.2658,3.6981,3.6981,2.5894,8.2475
4.6227,4.6227,3.2369,8.2292,5.5472,5.5472,3.8842,8.2110,6.4717,6.4717
4.5314,8.1927,7.3962,7.3962,5.1788,8.1745,8.3210,8.3210,5.8263,8.1562
10.7995,10.7995,13.1492,15.7096,11.9996,11.9996,13.8991,16.3313,13.1997,13.1997
14.6489,16.9531,14.3997,14.3997,15.3985,17.5750,15.5993,15.5993,16.1485,18.1968
16.7996,16.7996,16.8983,18.8185,17.9997,17.9997,17.6480,19.4402,19.1996,19.1996
18.3980,20.0622,20.3994,20.3994,19.1478,20.6840,21.5995,21.5995,19.8976,21.3059
0,0,3.5915,7.1831,1.1971,1.1971,4.5960,8.0080,2.3942,2.3942
5.6005,8.8330,3.5915,3.5915,6.6051,9.6576,4.7887,4.7887,7.6097,10.4827
5.9857,5.9857,8.6141,11.3079,7.1831,7.1831,9.6189,12.1330,8.3802,8.3802
10.6232,12.9579,9.5774,9.5774,11.6280,13.7826,10.7746,10.7746,12.6323,14.6077
0,0,2.0801,6.2406,0.9243,0.9243,2.7276,6.5553,1.8487,1.8487
3.375,6.8698,2.7736,2.7736,4.0222,7.1844,3.6981,3.6981,4.6697,7.4987
4.6227,4.6227,5.3171,7.8133,5.5472,5.5472,5.9643,8.1280,6.4717,6.4717
6.6118,8.4425,7.3962,7.3962,7.2593,8.7571,8.3210,8.3210,7.9067,9.0712
wing_area = 2000.0
wing_span = 141.73
wing_root_chord = 42.0
wing_dihedral = 6.2
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 32.0
wing_pos_apex_lon = 20.0
wing_pos_apex_vert = 0.0
htail_area = 1090.0
htail_span = 70.7
htail_pos_lon = -100.0
htail_pos_vert = 0.0
htail_incidence = 0.0
htail_sweep = 40.0
vtail_area = 573.0
vtail_span = 27.3
vtail_sweep = 35.0
vtail_pos_lon = -108.3
vtail_pos_vert = 5.8
elevator_area = 137.0
aileron_area = 68.0
rudder_area = 232.0
elevator_up_limit = 26.0
elevator_down_limit = 30.0
aileron_up_limit = 30.0
aileron_down_limit = 15.0
rudder_limit = 25.0
elevator_trim_limit = 20.0
spoiler_limit = 60.0
aileron_to_spoileron_gain = 3
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
spoilerons_available = 1

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 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, 17

[Flight_Tuning]
cruise_lift_scalar=1.6 
parasite_drag_scalar=1.8 
induced_drag_scalar=0.1 
elevator_effectiveness=1.0 
aileron_effectiveness=1.0 
rudder_effectiveness=1.0 
pitch_stability=0.8 
roll_stability=1.0 
yaw_stability=1.0 
elevator_trim_effectiveness=1.0 
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 

[TurbineEngineData]
fuel_flow_gain=0.002 
inlet_area=113.0 
rated_N2_rpm=29920 
static_thrust=16000 
afterburner_available=0 
reverser_available=1 

[Jet_Engine]
thrust_scalar=0.6 

[Brakes]
parking_brake    = 1
toe_brakes_scale = 0.1
[Flaps.0]
type             = 1
span-outboard    = 0.8
extending-time   = 8
lift_scalar      = 1.0
drag_scalar      = 1.0
pitch_scalar     = 1.0
flaps-position.0 = 0
flaps-position.1 = 17
flaps-position.2 = 17
flaps-position.3 = 26
flaps-position.4 = 32
flaps-position.5 = 32
damaging-speed   = 250
blowout-speed    = 300
system_type      = 1

[Flaps.1]
type             = 2
span-outboard    = 0.8
extending-time   = 2
lift_scalar      = 1.0
drag_scalar      = 1.0
pitch_scalar     = 1.0
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed   = 250
blowout-speed    = 300
system_type      = 1

[Pitot_Static]
vertical_speed_time_constant=1

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle
[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2
[Views]
eyepoint=90.0, -2.65, 8.89 

[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 

[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=3,0 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=1 
autothrottle_arming_required= 1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 1
pitch_takeoff_ga=8 ;
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=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[stall_warning]
type=2