[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"\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]
empty_weight=29800	// Empty weight of aircraft DOW (lbs)
reference_datum_position=0,0,0	// (feet) distance from FS Reference: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0,0,0 	// (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50	// Payload  weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.0=379,31,0,0	// Weight Pilots (lbs)
station_load.1=190,27,0,0	// Weight stewards in front (lbs)
station_load.2=190,-19,0,0	// Weight stewards in rear (lbs)
station_load.3=331,20.5,0,0	// Weight cargo 1 (lbs)
station_load.4=776,-23,0,0	// Weight cargo 2 (lbs)


station_load.5=190,16.1,0,0	// Weight passengers row 1 (lbs)
station_load.6=758,13.6,0,0	
station_load.7=569,11,0,0	
station_load.8=569,8.4,0,0	
station_load.9=569,5.8,0,0
station_load.10=758,3.2,0,0
station_load.11=379,0.6,0,0
station_load.12=569,-1.9,0,0
station_load.13=569,-4.5,0,0
station_load.14=569,-7.1,0,0
station_load.15=569,-9.7,0,0
station_load.16=379,-12.3,0,0
station_load.17=758,-14.9,0,0
station_load.18=190,-17.4,0,0

//The Zero Fuel Weight of this aircraft is 17600 kg equal 38801 pounds

// Moment of Inertia
empty_weight_roll_MOI=309051
empty_weight_pitch_MOI=800733
empty_weight_yaw_MOI=503747
empty_weight_coupled_MOI=0
max_gross_weight=44900
CG_forward_limit=0.000
CG_aft_limit=1.000

[Reference Speeds]
flaps_up_stall_speed=98.000000
full_flaps_stall_speed=78.000000
cruise_speed=287.000
max_indicated_speed=224.000000
max_mach=0.556982

[pitot_static]
vertical_speed_time_constant=2.0	// Increasing this value will cause a faster reaction in the VSI

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.0
aileron_effectiveness=1.20
rudder_effectiveness=1.400
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=5
Engine.0=7.620,-12.190,2.540
Engine.1=7.620,12.190,2.540
fuel_flow_scalar=0.75
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.005
inlet_area=2.100
rated_N2_rpm=29920.000
static_thrust=300.000
afterburner_available=0

[turboprop_engine]
power_scalar=1.0
maximum_torque=11124.000
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar=1.25
propeller_type=0
propeller_diameter=13.280
propeller_blades=4
propeller_moi=80.000
beta_max=45.0
beta_min=11.500
min_gov_rpm=24994.000
prop_tc=0.002
gear_reduction_ratio=24.686400
fixed_pitch_beta=0.000
low_speed_theory_limit=80.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=350.000
beta_feather=79.300
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=0.000
minimum_reverse_beta=-20.000

[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
electric_pump=0

[airplane_geometry]
wing_area=780.000
wing_span=95.120
wing_root_chord=11.200
wing_dihedral=2.500
wing_incidence=2.500
wing_twist=-0.967
oswald_efficiency_factor=0.750
wing_winglets_flag=0
wing_sweep=6.000
wing_pos_apex_lon=1.000
wing_pos_apex_vert=5.100
htail_area=149.000
htail_span=32.520
htail_pos_lon=-37.600
htail_pos_vert=4.100
htail_incidence=0.000
htail_sweep=10.000
vtail_area=186.000
vtail_span=14.103
vtail_sweep=25.000
vtail_pos_lon=-33.030
vtail_pos_vert=5.100
elevator_area=35.600
aileron_area=59.400
rudder_area=56.000
elevator_up_limit=30.000
elevator_down_limit=20.000
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=30.00
elevator_trim_limit=15.000
spoiler_limit=90.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[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,-7.6,1600, 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

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=15.0     //Flap angle that activates warning at idle
flap_limit_power=30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1       //Parking brake available
toe_brakes_scale=1.0  //Brake scalar

[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0         //no electric pumps
engine_map=1,1,0,0   //pumps on Eng1,2

[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

[autopilot]
autopilot_available=0
flight_director_available=0
default_vertical_speed=800.000000
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

[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

[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]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[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=17.40, -1.76, 2.04    //(feet) longitudinal, lateral, vertical distance from reference datum
eyepoint=18.13, -1.66, 2.04  

[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

[stall_warning]
type=2