[fltsim.0]
title=IL76 
sim=IL_76
model=
panel=
sound=
texture= 
kb_checklists=
kb_reference=
atc_id=
atc_airline= 
atc_flight_number=
atc_heavy=
atc_parking_types=CARGO
ui_manufacturer=IL
ui_type=Il-76TD (Varnavskiy)
ui_variation=Cargo 
description="IL76 Cargo"
atc_id_color=0x00000000
atc_id_font=
visual_damage=0
description= 


[General]
atc_type=IL 
atc_model= 
editable=1 
performance=" "
Category=airplane

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[weight_and_balance]

// ACM V2.5
max_gross_weight = 585000.000
empty_weight = 277000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI = 20000000.000
empty_weight_roll_MOI = 10000000.000
empty_weight_yaw_MOI = 26000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 11

station_load.0 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.1 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.2 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.3 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.4 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.5 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.6 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.7 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.8 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.9 = 0.000000, 0.000000, 0.000000, 0.000000
station_load.10 = 0.000000, 0.000000, 0.000000, 0.000000



[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.000
min_throttle_limit = -0.25
engine.0 = 3.000, -45.500, 2.000 
engine.1 = 14.000, -24.500, 4.000 
engine.2 = 14.000, 24.500, 4.000 
engine.3 = 3.000, 45.500, 2.000 

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
contrail=fx_contrail_l

    
[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0

Center1 = 0.000, 0.000, -7.000, 11424.000, 0.000
LeftMain = 0.000, -28.000, 10.000, 8000.000, 0.000
RightMain = 0.000, 28.000, 10.000, 8000.000, 0.000


[CONTACT_POINTS]
point.0=1, 40.344,   0.0,  -5.3, 1300.000, 0, 2.05, 50.00, 0.829, 2.5, 0.90, 16.0, 20.0, 0, 215.0, 270.0
point.1=1, -6.527,  -9.6,  -5.7, 2000.803, 1, 2.46,  0.00, 0.829, 2.5, 0.90, 16.0, 20.0, 2, 215.0, 270.0
point.2=1, -6.527,   9.6,  -5.7, 2000.803, 2, 2.46,  0.00, 0.829, 2.5, 0.90, 16.0, 20.0, 3, 215.0, 270.0
point.3=2, -70.62,   0.0, 12.75, 1574.803, 0, 0.00,  0.00, 0.000, 0.0, 0.00, 0.00, 0.00, 9,   0.0,   0.0
point.4=2,  54.87,   0.0, 0.065, 1574.803, 0, 0.00,  0.00, 0.000, 0.0, 0.00, 0.00, 0.00, 4,   0.0,   0.0
point.5=2, -25.16, 86.26, 7.216, 1574.803, 0, 0.00,  0.00, 0.000, 0.0, 0.00, 0.00, 0.00, 6,   0.0,   0.0
point.6=2, -25.16,-86.26, 7.216, 1574.803, 0, 0.00,  0.00, 0.000, 0.0, 0.00, 0.00, 0.00, 5,   0.0,   0.0
static_pitch=0.004
static_cg_height=5.33
max_number_of_points=10
gear_system_type=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]
//ACM_AREAW1// 0,0,0,11.4794,2.7939,2.7939,1.5487,12.3423,5.3643,5.3643
//ACM_AREAW2// 3.0974,12.9816,8.2701,8.2701,4.6462,13.2854,11.1759,11.1759,6.1949,13.9246
//ACM_AREAW3// 13.9700,13.9700,7.7436,14.4521,16.6521,16.6521,9.2924,15.0914,19.2225,19.2225
//ACM_AREAW4// 10.8411,15.6188,22.1283,22.1283,12.3899,16.2581,25.0341,25.0341,13.9386,16.7856
//ACM_AREAH1// 0,0,0,5.9330,1.1006,1.1006,0.6877,6.4024,2.2013,2.2013
//ACM_AREAH2// 1.3755,6.6481,3.3020,3.3020,2.0633,7.0057,4.2908,4.2908,2.7510,7.1396
//ACM_AREAH3// 5.5033,5.5033,3.4388,7.3853,6.6040,6.6040,4.1266,7.7429,7.8164,7.8164
//ACM_AREAH4// 4.8144,8.1005,8.6935,8.6935,5.5021,8.3462,9.9060,9.9060,6.1899,8.5920
//ACM_AREAV1// 0,0,0,8.7778,1.0498,1.0498,0.8809,9.5738,1.9879,1.9879
//ACM_AREAV2// 1.7618,10.7053,3.0377,3.0377,2.6428,11.6131,4.1994,4.1994,3.5237,12.6328
//ACM_AREAV3// 5.1375,5.1375,4.4047,13.7643,6.2992,6.2992,5.2856,14.4485,7.3490,7.3490
//ACM_AREAV4// 6.1665,15.1327,8.5107,8.5107,7.0475,16.1524,9.5606,9.5606,7.9284,16.7247
//ACM_CAREAW1// 18.3881,18.3881,13.3800,15.1167,19.2259,19.2259,13.7070,15.3066,19.8401,19.8401
//ACM_CAREAW2// 13.8104,15.4965,20.5662,20.5662,14.1375,15.7982,21.1804,21.1804,14.4645,15.9881
//ACM_CAREAW3// 21.7945,21.7945,14.7916,16.0661,22.4087,22.4087,15.1186,16.2560,23.2466,23.2466
//ACM_CAREAW4// 15.2220,16.3341,23.8608,23.8608,15.5491,16.4122,25.0341,25.0341,15.9879,16.8257
//ACM_CAREAH1// 0.2236,0.2236,4.3084,6.2685,1.1006,1.1006,4.4370,6.4556,2.3131,2.3131
//ACM_CAREAH2// 4.6775,6.6428,3.4138,3.4138,5.3653,6.8300,4.4026,4.4026,5.7176,7.0172
//ACM_CAREAH3// 5.6151,5.6151,6.2935,7.6517,6.4921,6.4921,6.7576,7.7271,7.7046,7.7046
//ACM_CAREAH4// 7.1099,8.1379,8.4698,8.4698,7.4622,8.3251,9.6823,9.6823,7.8145,8.6241
//ACM_CAREAV1// -0.1118,-0.1118,5.6052,8.7640,1.1616,1.1616,6.5980,9.9380,2.0997,2.0997
//ACM_CAREAV2// 7.1434,10.5528,3.2614,3.2614,8.4717,12.0622,4.0876,4.0876,8.9053,12.3416
//ACM_CAREAV3// 5.1375,5.1375,9.8981,13.5155,6.2992,6.2992,10.8909,14.1304,7.3490,7.3490
//ACM_CAREAV4// 11.5481,15.0807,8.2871,8.2871,12.4291,15.8073,9.3369,9.3369,13.0864,16.4221
wing_area = 3900.000
wing_span = 165.000
wing_root_chord = 38.000
wing_dihedral = -4.500
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor = 0.700
wing_winglets_flag = 1
wing_sweep = 29.000
wing_pos_apex_lon = 27.000
wing_pos_apex_vert = 12.000
htail_area = 900.000
htail_span = 65.000
htail_pos_lon = -91.000
htail_pos_vert = 50.000
htail_incidence = 0.000
htail_sweep = 32.000
vtail_area = 900.000
vtail_span = 31.000
vtail_sweep = 40.000
vtail_pos_lon = -63.000
vtail_pos_vert = 16.000
elevator_area = 280.000
aileron_area = 200.000
rudder_area = 350.000
elevator_up_limit = 25.000
elevator_down_limit = 15.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 30.000
elevator_trim_limit = 20.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 10.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[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
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 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



[Views]
eyepoint=59.02, -2.45, 6.49              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[Reference Speeds]
flaps_up_stall_speed= 180.000 
full_flaps_stall_speed= 120.000 
cruise_speed= 400.000 
max_mach                = 0.77
max_indicated_speed     = 435.0                 //Red line (KIAS)

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000
induced_drag_scalar=1.000 
elevator_effectiveness=2.002 
aileron_effectiveness=2.002 
rudder_effectiveness=1.000 
pitch_stability=2.002 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=0.504 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[TurbineEngineData]
fuel_flow_gain= 0.500 
inlet_area= 60.000 
rated_N2_rpm= 29920.000 
static_thrust= 40440.000 
afterburner_available= 0 
reverser_available= 1.000 

[jet_engine]
thrust_scalar=1.000 

[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 = 0.50  //Brake scalar
auto_brakes=4

[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

[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 = 0.5                               ;Percent per second
exit_rate.1 = 0.1                               ;Percent per second

[stall_warning]
type=2
stick_shaker=1
[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0

[Flaps.0]
type= 1
span-outboard= 0.700
extending-time= 10.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 0.750
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.900
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 1.000, 0.000
flaps-position.3= 1.000, 0.000
flaps-position.4= 1.000, 0.000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1