[fltsim.0]
title=Antonov An-24RV
sim=Antonov An-24RV
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Antonov
ui_type=An-24-RV
ui_variation=Aeroflot
atc_id=RU478
visual_damage=1
description="The Legendary Russian Turboprop"\n(Patch 1)\nAn-24 is the most used short-range aircraft in the ex-USSR. First flight: september,1 1963. Hundreds are still in service.\n\nFSDS2 model by D.Samborski ([email protected])\nExterior painting by N.Samsonov ([email protected])\nInterior painting by M.Mysin ([email protected])\nPanel by V.Bocharnikov ([email protected])\nGauges by S.Gritsevsky (c) 2003


[General]
atc_type=Antonov
atc_model=24
performance=Cruise speed at FL150 : 450-475 km/h ( 243-256 kts )\nMax takeoff weight : 21 tons (52500 lbs)\nMax landing weight : 21 tons (52500 lbs)\nMax vertical speed at takeoff : 7.1 m/s\nEngines : 2x2550 hp Ivchenko AI-24 turboprops + 1x800kgs jet RU-19\n48 passengers

[WEIGHT_AND_BALANCE]
MTW=46666 //21000 kg
MLW=46666  //21000 kg
empty_weight=38000.000  //17100 kg with payload

reference_datum_position     =    0.0, 0, 0
empty_weight_CG_position     =  0, 0, 0

empty_weight_pitch_MOI = 1002439
empty_weight_roll_MOI = 2363372
empty_weight_yaw_MOI = 2588164
empty_weight_coupled_MOI=10000.000
max_gross_weight=46660.000      //21000kg
station_load.0=0.000000,0.000000,0.000000,0.000000


max_battery_voltage=27
generator_alternator_voltate=28.5
max_generator_alternator_amps=600.0

flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 15, 17.0
additional_system=0, 2 , 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
starter2=0, 20, 17.0
light_nav=0, 5 , 10.0
light_beacon=0, 5 , 10.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 10.0
light_panel=0, 5 , 10.0


[fuel]
LeftMain=1.000, -17.400, -1.860, 470.250, 0.000 //1426kg
LeftAux=0.000, -10.000, -1.860, 181.500, 0.000 //550kg
RightMain=1.000, 17.400, -1.860, 470.250, 0.000 //1426kg
RightAux=0.000, 10.000, -1.860, 181.5, 0.000 //550kg
fuel_type=2.000000
number_of_tank_selectors=2
electric_pump=0

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=2.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=0.500
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
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=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 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


[airplane_geometry]
//ACM_AREAW1// 0,0,0,4.8768,1.6227,1.6227,0,4.6329,3.2455,3.2455
//ACM_AREAW2// 0,4.3891,4.8683,4.8683,0,4.1452,6.4911,6.4911,0,3.9014
//ACM_AREAW3// 8.1138,8.1138,0,3.6576,9.7366,9.7366,0,3.4137,11.3594,11.3594
//ACM_AREAW4// 0,3.1699,12.9822,12.9822,0,2.9260,14.6050,14.6050,0,2.6822
//ACM_AREAH1// 0,0,0,3.8100,0.6349,0.6349,0,3.6195,1.2699,1.2699
//ACM_AREAH2// 0,3.4290,1.9050,1.9050,0,3.2385,2.5399,2.5399,0,3.0480
//ACM_AREAH3// 3.1750,3.1750,0,2.8575,3.8100,3.8100,0,2.6670,4.4450,4.4450
//ACM_AREAH4// 0,2.4765,5.0799,5.0799,0,2.2860,5.7150,5.7150,0,2.0954
//ACM_AREAV1// 0,0,0,6.5478,0.7275,0.7275,0,6.0240,1.4550,1.4550
//ACM_AREAV2// 0,5.5002,2.1826,2.1826,0,4.9763,2.9101,2.9101,0,4.4525
//ACM_AREAV3// 3.6377,3.6377,0,3.9287,4.3652,4.3652,0,3.4048,5.0927,5.0927
//ACM_AREAV4// 0,2.8810,5.8203,5.8203,0,2.3572,6.5478,6.5478,0,1.8334
//ACM_CAREAW1// 7.3025,7.3025,2.4384,3.4137,8.1138,8.1138,2.4384,3.3649,8.9252,8.9252
//ACM_CAREAW2// 2.4384,3.3162,9.7366,9.7366,2.4384,3.2674,10.5480,10.5480,2.4384,3.2186
//ACM_CAREAW3// 11.3594,11.3594,2.4384,3.1699,12.1708,12.1708,2.4384,3.1211,12.9822,12.9822
//ACM_CAREAW4// 2.4384,3.0723,13.7936,13.7936,2.4384,3.0236,14.6050,14.6050,2.4384,2.9748
//ACM_CAREAH1// 0,0,1.9050,3.8100,0.6349,0.6349,1.9050,3.7147,1.2699,1.2699
//ACM_CAREAH2// 1.9050,3.6195,1.9050,1.9050,1.9050,3.5242,2.5399,2.5399,1.9050,3.4290
//ACM_CAREAH3// 3.1750,3.1750,1.9050,3.3337,3.8100,3.8100,1.9050,3.2385,4.4450,4.4450
//ACM_CAREAH4// 1.9050,3.1432,5.0799,5.0799,1.9050,3.0480,5.7150,5.7150,1.9050,2.9527
//ACM_CAREAV1// 0,0,1.6369,4.9109,0.7275,0.7275,1.6369,4.6489,1.4550,1.4550
//ACM_CAREAV2// 1.6369,4.3870,2.1826,2.1826,1.6369,4.1251,2.9101,2.9101,1.6369,3.8632
//ACM_CAREAV3// 3.6377,3.6377,1.6369,3.6013,4.3652,4.3652,1.6369,3.3394,5.0927,5.0927
//ACM_CAREAV4// 1.6369,3.0775,5.8203,5.8203,1.6369,2.8155,6.5478,6.5478,1.6369,2.5536
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=0.600
extending-time=16.000
system_type=1
damaging-speed=162.000
blowout-speed=170.000
lift_scalar=3.50  //1.6
drag_scalar=1.9M 00   //0.5
pitch_scalar=1.00 //1.000
flaps-position.0=0.000, 0
flaps-position.1=5.000, 162.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0
flaps-position.4=20.000, 135.0
flaps-position.5=25.000, 0
flaps-position.6=30.000, 0
flaps-position.7=38.000, 0


[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
min_throttle_limit=-0.449890

[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=102.000000
full_flaps_stall_speed=82.000000
cruise_speed=223.0
max_indicated_speed=292.000000
max_mach=0.650000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[autopilot]
autopilot_available=0
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

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[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
point.7= 5, -30.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0,  0.0,       1.00, 8.0, 8.2, 0, 0.0, 0.0

static_pitch=0.00
static_cg_height=7.908113
gear_system_type=0

[exits]
number_of_exits = 2
exit_rate.0 = 0.053                             ;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

[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.075,0.075	                          ;Percent per second

[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 = 1, -37.53,  0.00, 9.21, fx_beaconb ,
light.3 = 1, -8.50,  0.00, -4.21, fx_beaconh,
light.4 = 3, -49.50,   0.00,  4.00, fx_navwhi ,
light.5 = 4, 19, 0, 0, fx_vclight
light.6 = 4, 17, -2, 0, fx_vclight

[Views]
eyepoint=18.0, -1.76, 2.04    //(feet) longitudinal, lateral, vertical distance from reference datum
//eyepoint=18.13, -1.36, 2.04    

[brakes]
toe_brakes_scale=1.220740
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0