[FLTSIM.0]
title=AI IL-76TD 76649
sim=ai76
model=a50
panel=
sound=
texture=33
kb_checklists=
kb_reference=
atc_id=76649
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Beriev
ui_type=A-50
ui_variation=76649
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.1]
title=AI IL-76TD 76668
sim=ai76
model=a50
panel=
sound=
texture=51
kb_checklists=
kb_reference=
atc_id=76668
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Beriev
ui_type=A-50
ui_variation=76668
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.2]
title=AI IL-76TD 76708
sim=ai76
model=md
panel=
sound=
texture=76708
kb_checklists=
kb_reference=
atc_id=76708
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=IL-76MD
ui_variation=76708
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.3]
title=AI IL-76TD 76741
sim=ai76
model=md
panel=
sound=
texture=76741
kb_checklists=
kb_reference=
atc_id=76741
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=IL-76MD
ui_variation=76741
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.4]
title=AI IL-76TD 76772
sim=ai76
model=md
panel=
sound=
texture=76772
kb_checklists=
kb_reference=
atc_id=76772
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=IL-76MD
ui_variation=76772
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
visual_damage=0
atc_parking_types=
atc_parking_codes=AF76
[FLTSIM.5]
title=AI IL-76TD RA76840
sim=ai76
model=a50
panel=
sound=
texture=52
kb_checklists=
kb_reference=
atc_id=76840
atc_flight_number=
atc_heavy=0
atc_airline=MCS
ui_manufacturer=Beriev
ui_type=A-50
ui_variation=RA76840
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=MC76
[FLTSIM.6]
title=AI IL-76TD 78745
sim=ai76
model=md
panel=
sound=
texture=78745
kb_checklists=
kb_reference=
atc_id=78745
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=IL-76MD
ui_variation=78745
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.7]
title=AI IL-76TD 78809
sim=ai76
model=md
panel=
sound=78809
texture=
kb_checklists=
kb_reference=
atc_id=78809
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=IL-76MD
ui_variation=78809
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.8]
title=AI IL-76TD 78840
sim=ai76
model=md
panel=
sound=
texture=78840
kb_checklists=
kb_reference=
atc_id=78840
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Ilyushin
ui_type=AI IL-76md
ui_variation=78840
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[FLTSIM.9]
title=AI IL-76TD 78764
sim=ai76
model=a50
panel=
sound=
texture=51
kb_checklists=
kb_reference=
atc_id=78764
atc_flight_number=
atc_heavy=0
atc_airline=AIR FORCE
ui_manufacturer=Beriev
ui_type=A-50
ui_variation=78764
description=Model by Varnavskiy Sergey ( [email protected] )\nPainting by Nikolai Samsonov (aka INS, [email protected])\nFlight Dynamics by Fedotov Alexander and Usachev Pavel (aka Usachev Pavel, [email protected])
atc_parking_types=
visual_damage=0
atc_parking_codes=AF76
[General]
atc_type=ILYUSHIN
atc_model=IL76
editable=0
performance=IL-76
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 905000 // (pounds)
empty_weight = 504088 // (pounds)
reference_datum_position = 83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0, -19.0, -2.0, 8.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, -19.0, 2.0, 8.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "1700.0, -83.5, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "5440.0, -27.0, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "5780.0, -65.0, 0.0, 0.0, Business Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "7140.0, -50.0, 0.0, 8.0, Upper Deck" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "10710.0, -91.0, 0.0, 0.0, Coach 1-7" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "18020.0, -119.0, 0.0, 0.0, Coach 8-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "23800.0, -160.0, 0.0, 0.0, Coach 19-34" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "18000.0, -52.0, 0.0, -6.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "6000.0, -123.0, 0.0, -6.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_roll_MOI = 13352310
empty_weight_pitch_MOI = 24223159
empty_weight_yaw_MOI = 39531785
empty_weight_coupled_MOI = 0
[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)
point.0 = 1, -25.0, 0.0, -13.9, 1000.0, 0, 2.0, 70.0, 1.0, 2.7, 0.900, 12.0, 12.0, 0, 220, 250
point.1 = 1, -114.0, -18.0, -13.9, 2000.0, 1, 2.0, 13.0, 1.0, 2.7, 0.900, 17.0, 15.0, 2, 220, 250
point.2 = 1, -114.0, 18.0, -13.9, 2000.0, 2, 2.0, 13.0, 1.0, 2.7, 0.900, 17.0, 15.0, 3, 220, 250
point.3 = 2, -152.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, -152.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, 3.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -222.7, 0.0, 4.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
static_pitch =0
static_cg_height = 15.5
gear_system_type=1 //Hydraulic
[fuel]
LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -193.5, 0.0, 6.0, 3300.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 5825.0 //Square feet
wing_span = 211.4 //Feet
wing_root_chord = 48.8 //Feet
wing_dihedral = 7.0 //Degrees
wing_incidence = 2.0 //Degrees
wing_twist = -1.0 //Degrees
oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing
wing_winglets_flag = 1 //Are winglets available?
wing_sweep = 37.5 //Degrees, wing leading edge
wing_pos_apex_lon = -58.2 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0 //Feet, vertical distance from reference point, positive going up
htail_area = 1470 //Square feet
htail_span = 72.8 //Feet
htail_pos_lon = -210.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 37.5 //Degrees, horizontal tail leading edge
vtail_area = 1060 //Square feet
vtail_span = 37.1 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -198.5 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up
elevator_area = 327 //Square feet
aileron_area = 225 //Square feet
rudder_area = 230 //Square feet
elevator_up_limit = 25 //Degrees
elevator_down_limit = 15 //Degrees
aileron_up_limit = 25 //Degrees
aileron_down_limit = 15 //Degrees
rudder_limit = 31.5 //Degrees
elevator_trim_limit = 20 //Degrees
spoiler_limit = 45 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 3 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 10 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 112.0 //Knots True (KTAS)
cruise_speed = 477.0 //Knots True (KTAS)
max_mach = 0.92
max_indicated_speed = 365.0 //Red line (KIAS)
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 10 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 200 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.9
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 2 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0.0 // degrees
flaps-position.2 = 1.0 // degrees
flaps-position.3 = 2.0 // degrees
damaging-speed = 180 // KIAS
blowout-speed = 220 // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1 //Hydraulic
[flight_tuning]
cruise_lift_scalar = 1.5
parasite_drag_scalar = 1.5
induced_drag_scalar = 1.5
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -92.00, -81.00, 4.00, fx_navred ,
light.1 = 3, -92.00, 81.00, 4.00, fx_navgre ,
light.2 = 1, -49.00, 0.00, 10.83, fx_beaconh ,
light.3 = 1, -130.22, 0.00, -0.70, fx_beaconb ,
light.4 = 7, -106.6, -38.0, -1.8, fx_smoke_Il76
light.5 = 7, -70.3, -20.5, -2.8, fx_smoke_Il76
light.6 = 7, -70.3, 20.5, -2.8, fx_smoke_Il76
light.7 = 7, -106.6, 38.0, -1.8, fx_smoke_Il76
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 6.5, -69.5, -1.9 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 7.0, -38.9, -2.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 7.0, 38.9, -2.4 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = 6.5, 69.5, -1.9 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.4; //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 60.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 56750 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[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=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
[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
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.24 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[Views]
eyepoint = -19.05, -1.97, 9.7 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 5 , 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[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
[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.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=SKJ_fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[stall_warning]
type=2
