[fltsim.0]
title=Turkmenistan Airlines Antonov An-24
sim=Antonov An-24RV-traffic
model=
panel=
sound=
texture=Turkmenistan
checklists=
atc_airline=
ui_manufacturer=AI
ui_type=An-24-RV-traffic
ui_variation=Turkmenistan Airlines
description="legendary russian turboprop"
atc_id=EZ-2405
atc_parking_types=GATE
atc_parking_codes=TUA


[General]
atc_type=ANTONOV
atc_model=AN24
editable=0
performance=

[WEIGHT_AND_BALANCE]
max_gross_weight=34500                        // (pounds)
empty_weight=22730                            // (pounds)

reference_datum_position=31.0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-26.0, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50

station_load.0=170,  -9.8, -1.75, 0.0         //Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  -9.8,  1.75, 0.0         //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=5660, -27.0,  0.0, 0.0         //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=111701
empty_weight_roll_MOI=61201
empty_weight_yaw_MOI=161691
empty_weight_coupled_MOI=0


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

[GeneralEngineData]
engine_type=5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-28.4, -13.3, 2.7                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-28.4,  13.3, 2.7                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000

[propeller]
thrust_scalar=1.0                   //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13.0                  //Propeller Diameter, (feet)
propeller_blades=4                     //Number of propeller blades
propeller_moi=77                    //Propeller moment of inertia
beta_max=45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520                 //Miminum governed RPM
prop_tc=0.004                 //Prop time-constant
gear_reduction_ratio=17.0                  //Propeller gear reduction ratio
fixed_pitch_beta=0                     //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                    //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1                     //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                     //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=700                   //Minimum RPM for prop feathering
beta_feather=79.3                  //Feathering pitch angle (degrees)
power_absorbed_cf=0.9                   //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=200                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=7878                  //Maximum torque available (ft-lbs)

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
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, 2 , 17.0
additional_system=0, 20, 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
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

[Views]
eyepoint=-8.8, -1.45, 2.1      //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=5                                    // seconds
flaps-position.0=0                                    // degrees, KIAS
flaps-position.1=10                                   // degrees, KIAS
flaps-position.2=30                                   // degrees, KIAS
flaps-position.3=40                                   // degrees, KIAS
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS

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

[fuel]
LeftMain=-31.1, -9.1, 3.9, 417.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-31.1,  9.1, 3.9, 417.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1                    
electric_pump=0

[airplane_geometry]
wing_area=585.0                 //Square feet
wing_span=85.0                  //Feet
wing_root_chord=7.0                   //Feet
wing_dihedral=2.5                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-3.0                  //Degrees
oswald_efficiency_factor=0.7                   //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=3.0                   //Degrees, wing leading edge
wing_pos_apex_lon=-25.0                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=97.0                  //Square feet
htail_span=26.0                  //Feet
htail_pos_lon=-58.9                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=1.0                   //Degrees
htail_sweep=8.0                   //Degrees, horizontal tail leading edge
vtail_area=106.0                 //Square feet
vtail_span=11.7                  //Feet, tip to body
vtail_sweep=30.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-54.9                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.4                   //Feet, vertical distance from reference point, positive going up
elevator_area=53.5                  //Square feet
aileron_area=12.1                  //Square feet
rudder_area=46.4                  //Square feet
elevator_up_limit=17.0                  //Degrees
elevator_down_limit=15.5                  //Degrees
aileron_up_limit=18.0                  //Degrees
aileron_down_limit=18.0                  //Degrees
rudder_limit=30.0                  //Degrees
elevator_trim_limit=15.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=0                     //Spoilerons Available?
aileron_to_spoileron_gain=0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=0                 //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=92.0                  //Knots True (KTAS)
full_flaps_stall_speed=72.0                  //Knots True (KTAS)
cruise_speed=265.0                 //Knots True (KTAS)
max_indicated_speed=265.000000
max_mach=0.579980

[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[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

[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,-12.00, 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,-39.00,-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,-39.00,12.50,-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,-34.916667,-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,-34.916667,46.500000,4.416667,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,6.00,0.00,0.00
point.5=2.00,-75.750000,0.00,2.00,1574.803150,0.00,0.00,0.00,0.00,0.00,0.00,0.00,0.00,9.00,0.00,0.00
point.6=2.00,-9.333333,0.00,-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=7.9          //feet, altitude of CG when at rest on the ground

max_number_of_points=21
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, -36.96,-47.67, 3.24, fx_navredm ,
light.1=3, -36.96, 47.67, 3.24, fx_navgrem ,
light.2=2, -68.53,  0.00, 9.21, fx_beaconb ,
light.3=2, -39.50,  0.00, -4.21, fx_beaconh,
light.4=3, -80.50,   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 ,
[brakes]
toe_brakes_scale=1.062532
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[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