[fltsim.0]
title=Antonov AN124-210
sim=an124
model=
panel=
sound=
texture=
checklists=
description=Antonov AN124-210 Heavy Lift Cargo Jet.\nAdvanced version of the AN124-100.\nHigher Service ceiling, Longer range, and more power.\nUpdated and corrected Flight Dynamics by:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nArlington, Texas (USA)\nKC6ZOF@Yahoo.com\nJanuary 2009\n
ui_manufacturer=Antonov
ui_type=AN124-210
ui_variation=Antonov design bureau
atc_heavy=1
atc_id=UR_82072
atc_airline=Antonov
atc_flight_number=2072
atc_parking_types=CARGO
[General]
performance=Engines: 4 Rolls-Royce RB211-524H-T, 60,600 lbf each\nLength: 69.10 m (226.46 ft)\nHeight: 21.08 m (69.1 ft)\nWing span: 73.3 m (240.485083 ft)\nWing area: 628.0 m² (6,760 ft²)\nEmpty Weight: 175,000 kg (385,805 lbs)\nMTOW: 405,000 kg (892,863 lbs)\nPayload: 17,649 kg (38,909 lbs)\nFuel capacity: 69,873 US gal\nMmo: 0.985\n\nExpected Range:\n\nHigh Speed:\n5,800 nm @ FL500W, mach .97\n6,600 nm @ FL510E, mach .97\n\nEconomy:\n6,500 nm @ FL400W, mach .84\n7,900 nm @ FL410E, mach .84\n\nService Ceiling: 15,700 m (51,509 ft)\nCrew: 6 (pilot, co-pilot, navigator, communication operator, engineer, electrical engineer)\n
atc_type=Antonov
atc_model=AN124
Category=airplane
editable=1
[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]
max_gross_weight=892863.0
empty_weight=385805.0
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
//payload = 38,909 lbs
station_load.0=170.0,100.0,-4.0,12.5,
station_load.1=170.0,100.0,4.0,12.5,
station_load.2=680.0,80.0,0.0,12.5,
station_load.3=18437.0,56.5,0.0,-10.0,
station_load.4=9726.0,-37.5,0.0,-10.0,
station_load.5=9726.0,-75.0,0.0,-10.0,
;Moments of Inertia
empty_weight_roll_MOI= 13352310.000
empty_weight_pitch_MOI= 24223159.000
empty_weight_yaw_MOI= 39531785.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
//69,873 US gal = 468,149 lbs
LeftMain=-12.000, -40.000, 4.000, 23300.000, 0.000
RightMain=-12.000, 40.000, 4.000, 23300.000, 0.000
LeftAux=-28.400, -80.000, 3.000, 11636.500, 0.000
RightAux=-28.400, 80.000, 3.000, 11636.500, 0.000
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[GeneralEngineData]
engine_type= 1
Engine.0= -2.000, -59.100, -2.600
Engine.1= -18.400, -33.500, -4.300
Engine.2= -18.400, 33.500, -4.300
Engine.3= -2.000, 59.100, -2.600
fuel_flow_scalar= 1.000
min_throttle_limit=-0.25;
[SMOKESYSTEM]
smoke.0= -20.000, -59.100, -2.600, fx_smoke_f6
smoke.1=-38.400, -33.500, -4.300, fx_smoke_f6
smoke.2=-38.400, 33.500, -4.300, fx_smoke_f6
smoke.3= -20.000, 59.100, -2.600, fx_smoke_f6
[TurbineEngineData]
fuel_flow_gain= 0.002
bypass_ratio=4.4
inlet_area=17.6083
rated_N2_rpm=29920.0
static_thrust=60600.0
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.0
[airplane_geometry]
wing_area=6760.0
wing_span=240.485083
wing_root_chord= 48.800
wing_dihedral=-7.000
wing_incidence= 2.000
wing_twist= -1.000
oswald_efficiency_factor= 0.580
wing_winglets_flag= 0
wing_sweep= 37.500
wing_pos_apex_lon= 1.000
wing_pos_apex_vert= 10.000
htail_area=2038.4
htail_span= 72.800
htail_pos_lon= -121.400
htail_pos_vert= 10.000
htail_incidence= 0.000
htail_sweep= 37.500
vtail_area=1038.8
vtail_span= 37.100
vtail_sweep= 45.000
vtail_pos_lon= -120.500
vtail_pos_vert= 26.100
elevator_area= 527.000
aileron_area= 325.000
rudder_area= 330.000
elevator_up_limit= 25.000
elevator_down_limit= 15.000
aileron_up_limit= 25.000
aileron_down_limit= 25.000
rudder_limit= 25.500
elevator_trim_limit= 20.000
spoiler_limit= 40.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000
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
[Reference Speeds]
flaps_up_stall_speed= 130.000
full_flaps_stall_speed= 102.000
cruise_speed=430
max_mach=0.985
max_indicated_speed=365.0 //Red line (KIAS)
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=0.7
aileron_effectiveness=0.5
rudder_effectiveness=0.5
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=0.7
aileron_trim_effectiveness=0.5
rudder_trim_effectiveness=0.5
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=110
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
[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= 1.000, 51.500, 0.000, -20.300, 1000.000, 0.000, 3.000, 70.000, 1.500, 1.500, 0.900, 12.000, 12.000, 0.000, 200.000, 388.253
point.1= 1.000, -35.400, -13.500, -20.500, 3000.000, 1.000, 3.500, 13.000, 1.000, 2.500, 0.900, 15.000, 15.000, 2.000, 200.000, 388.253
point.2= 1.000, -35.400, 13.500, -20.500, 3000.000, 2.000, 3.500, 13.000, 1.000, 2.500, 0.900, 15.000, 15.000, 3.000, 200.000, 388.253
point.3= 2.000, 84.300, 0.000, -6.200, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 58.400, 0.000, 12.800, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -13.100, 0.000, 50.500, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, -144.700, 0.000, 8.900, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, -79.100, 0.000, -13.100, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8= 2.000, 56.100, 0.000, -15.400, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9= 2.000, -48.200, 121.400, 3.600, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.10= 2.000, -48.200, -121.400, 3.600, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.11= 2.000, -140.100, 44.300, 6.900, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.12= 2.000, -140.100, -44.300, 6.900, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -1.500
static_cg_height= 18.600
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=0 //Off
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
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
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.5=2, -144.4, 0.00, 8.2, fx_strobeh ,
light.6=1, 35.1, 0.00, 12.9, fx_beaconh ,
light.7=1, 44.2, 0.00, -15.1, fx_beaconb ,
light.8=4, 59.7, 0.00, 11.2, fx_vclighth,
[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=fx_tchdwn, 1
[exits]
number_of_exits=2
exit_rate.0=0.2 ;Percent per second
exit_rate.1=0.05 ;Percent per second
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9
[folding_wings]
wing_fold_system_type=4
fold_rates=0.11,0.13 ;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
stick_shaker=1
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 310.000
blowout-speed= 350.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
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= 0.300
extending-time= 8.000
system_type= 1
damaging-speed= 310.000
blowout-speed= 350.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 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
