[fltsim.0]
title=Antonov An-24B
sim=Antonov An-24B
model=b-light
panel=
sound=
texture=b80
checklists=
ui_manufacturer=Antonov
ui_type=An-24-B
ui_variation=Aeroflot classic 80-s
description="The Legendary Soviet Turboprop". Classical Aeroflot livery in the 80-s. The most popular soviet short-range commuter. Production: 1962-1978. More than 1200 built
[fltsim.1]
title=Antonov An-24B 70-special
sim=Antonov An-24B
model=b-light
panel=
sound=
texture=b70x
checklists=
ui_manufacturer=Antonov
ui_type=An-24-B
ui_variation=Aeroflot 70-s special
description="The Legendary Soviet Turboprop". Rare Aeroflot livery in the 70-s. The most popular soviet short-range commuter. Production: 1962-1978. More than 1200 built
[fltsim.2]
title=Antonov An-24B 70-s
sim=Antonov An-24B
model=b-light
panel=
sound=
texture=b70
checklists=
ui_manufacturer=Antonov
ui_type=An-24-B
ui_variation=Aeroflot 70-s
description="The Legendary Soviet Turboprop". Rare Aeroflot livery in the 70-s. The most popular soviet short-range commuter. Production: 1962-1978. More than 1200 built
[fltsim.3]
title=Antonov An-24B Zhar Ptitsa
sim=Antonov An-24B
model=b-light
panel=
sound=
texture=b60
checklists=
ui_manufacturer=Antonov
ui_type=An-24-B
ui_variation=Aeroflot 60-s "Zhar Ptitsa"
description="The Legendary Soviet Turboprop". One of the first liveries. Only three aircrafts were painted this way. The most popular soviet short-range commuter. Production: 1962-1978. More than 1200 built
[General]
performance=Cruise speed 460 km\/h\nMTOW 21000 kg\nLength 24.3m\nWingspan 29.2m\n\nFirst Flight : 1964
[WEIGHT_AND_BALANCE]
;Place for comments
empty_weight = 29800
reference_datum_position = 0.0, 0, 0
empty_weight_CG_position = -1.79, 0, 0
empty_weight_roll_MOI=2363372.000000
empty_weight_pitch_MOI=3172439.000000
empty_weight_yaw_MOI=2588164.000000
empty_weight_coupled_MOI=0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
[fuel]
LeftMain=0.000000,0.000000,0.000000,733.000000,0.000000
RightMain=0.000000,0.000000,0.000000,733.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area=804 // 1531.000000
wing_span=95.833333
wing_root_chord=16.000000
wing_dihedral=-0.999512
wing_incidence=0.247192
wing_twist=0.999756
oswald_efficiency_factor=2.695767
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=323.000000
htail_span=37.500000
htail_pos_lon=-42.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=355.000000
vtail_span=21.482551
vtail_sweep=0.000000
vtail_pos_lon=-38.416667
vtail_pos_vert=5.833333
elevator_area=45.750000
aileron_area=35.400000
rudder_area=29.240000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=10.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=15,0.000000
flaps-position.2=38,0.000000
[GeneralEngineData]
engine_type=1
Engine.0=6.000000,-12.750000,4.916667
Engine.1=6.000000,12.750000,4.916667
fuel_flow_scalar=1.000000
[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=6.132120
rated_N2_rpm=29920.000000
static_thrust=4100.100000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=105.000000
full_flaps_stall_speed=84.000000
cruise_speed=223.041725
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
[direction_indicators]
direction_indicator.0=3,0
[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=1.00,19.00, 0.00,-7.8,1600, 0.00, 1.1, 45.0, 0.80, 1.700000, 0.95, 6.00,6.00, 0.00, 0.00,0.00
point.1=1.00,-8.00,-12.5,-7.8,1800, 1.00, 1.6, 0.00, 0.75, 1.200000, 0.43, 7.00,7.00, 2.00, 0.00,0.00
point.2=1.00,-8.00,12.50,-7.8,1800, 2.00, 1.6, 0.00, 0.75, 1.200000, 0.43, 7.00,7.00, 3.00, 0.00,0.00
point.3=2.00,-3.916667,-46.500000,4.416667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,5.00,0.00,0.00
point.4=2.00,-3.916667,46.500000,4.416667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.5=2.00,-44.750000,0.00,2.00,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.6=2.00,22.333333,0.00,-2.500000,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,4.00,0.00,0.00
static_pitch=0.00
static_cg_height=7.908113
[exits]
number_of_exits = 2
exit_rate.0 = 0.09 ;Percent per second
exit_rate.1 = 0.2 ;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 = 1.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -5.96,-47.67, 3.24, fx_navredm ,
light.1 = 3, -5.96, 47.67, 3.24, fx_navgrem ,
light.2 = 2, -37.53, 0.00, 9.21, fx_beaconb ,
light.3 = 2, -8.50, 0.00, -4.21, fx_beaconh,
light.4 = 3, -49.50, 0.00, 4.00, fx_navwhi ,
//light.5 = 4, 18.13, 0.00, 2.3, fx_vclighth ,
//light.6 = 5, -2.00, 3.7, 26.42, fx_landing ,
//light.7 = 5, -2.00, 3.7, -26.42, fx_landing ,
[Views]
eyepoint=18.13, -1.36, 2.04 //(feet) longitudinal, lateral, vertical distance from reference datum
