[fltsim.0]
title=Turkmenistan Airlines Boeing B757-200
sim=aia_757_200_RR
model=RR
panel=
sound=RR
texture=turkmenistan
kb_checklists=
kb_reference=
atc_id=EZ-A014
atc_airline=TURKMENISTAN AIRLINES
atc_flight_number=701
ui_manufacturer=AI
ui_type=Boeing 757-200
ui_variation=Turkmenistan Airlines
description=AI Aardvark 757-200 (RR)
atc_id_color=0000000000
atc_heavy=1
visual_damage=0
atc_parking_types=GATE
atc_parking_codes=TUA




[General]
atc_type=Boeing 
atc_model=B752 
editable=1 
performance=Only experienced AI pilots should attempt to fly this aircraft. 
TBAirCraftFolderUId=11

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI

[weight_and_balance]

// ACM V1.0 pl4
max_gross_weight=120000
empty_weight=90792
reference_datum_position=0, 0, 0
empty_weight_CG_position=0, 0, 0
empty_weight_pitch_MOI=3172439
empty_weight_roll_MOI=2262183
empty_weight_yaw_MOI=3337024
empty_weight_coupled_MOI=0
max_number_of_stations=50

station_load.0=0.000000,0.000000,0.000000,0.000000


[flight_tuning]
cruise_lift_scalar=.600 
parasite_drag_scalar=.550 
induced_drag_scalar=.550 
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=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=4.75, -16.1, -2.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=4.75,  16.1, -2.5                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1                            //Scalar for fuel flow efficiency
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=19000                           //Lbs, max rated static thrust at Sea Level
afterburner_available=0                       //Afterburner available?
reverser_available=1                         //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0

[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 
//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)

[contact_points]
static_pitch=-0.2
static_cg_height=10
max_number_of_points=7

point.0=1, 54.8838, 0, -11.5112, 1181.1, 0, 1.442, 55.92, 0.8, 2.5, 0.9, 4, 4, 0, 0, 0
point.1=1, -10.0004, -12.1997, -11.1777, 1574.8, 1, 1.442, 0, 1, 2.5, 0.9, 6.9, 6.9, 2, 0, 0
point.2=1, -10.0004, 12.1997, -11.1777, 1574.8, 2, 1.442, 0, 1, 2.5, 0.9, 7.1, 7.1, 3, 0, 0
point.3=2, -14.17, -63.2621, 3.7485, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, -14.17, 62.3252, 4.6859, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5=2, -86.1915, 0, 5.5721, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6=2, 74.8857, 0, 0.5801, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
gear_system_type=0


[Views]
eyepoint=43.7, -1.31, 3.55   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=20                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=1                                    // degrees
flaps-position.2=2                                    // degrees
flaps-position.3=5                                    // degrees
flaps-position.4=10                                   // degrees
flaps-position.5=15                                   // degrees
flaps-position.6=25                                   // degrees
flaps-position.7=30                                   // degrees
flaps-position.8=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[flaps.1]       //Inboard Leading Edge Flaps
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=2                                    // seconds
flaps-position.0=0                                    // 
flaps-position.1=1.0                                  // 
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.875
drag_scalar=1.200
pitch_scalar=0.875
system_type=1                                         //Hydraulic

[flaps.2]       //Outboard Leading Edge Slat
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=3                                    // seconds
flaps-position.0=0                                    // 
flaps-position.1=0.5                                  // 
flaps-position.4=1.0                                  // 
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[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.0=3, -17.57, -62.91, 5.5, fx_navredm
light.1=3, -17.57, 62.91, 5.5, fx_navgrem
light.2=2, -17.01, -62.79, 5.5, fx_strobeh
light.3=2, -17.01, 62.79, 5.5, fx_strobeh
light.4=2, -0.72, 0, -4.13, fx_beaconb
light.5=1, 51.76, 0, 10.89, fx_beaconh
light.6=3, -22.14, 62.54, 5.67, fx_navwhih
light.7=3, -22.14, -62.54, 5.67, fx_navwhih


[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 

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

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

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800 
autothrottle_available=1 
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8 ;
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

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type=2
number_of_tank_selectors=1

Center1=0, 0, 0, 2313, 0
LeftMain=-3, -19, 0, 1500, 0
RightMain=-3, 19, 0, 1500, 0
electric_pump=0


[airplane_geometry]
wing_area=1160.0                //Square feet
wing_span=94.75              //Feet 
wing_root_chord=18.0                  //Feet
wing_dihedral=6.2                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-0.5                  //Degrees
oswald_efficiency_factor=0.75                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=25.0                  //Degrees, wing leading edge
wing_pos_apex_lon=8.0                   //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=338.0                 //Square feet
htail_span=41.7                  //Feet
htail_pos_lon=-35.0                 //Feet35.0, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0                   //Degrees
htail_sweep=30.0                  //Degrees, horizontal tail leading edge
vtail_area=224.0                 //Square feet
vtail_span=20.0                  //Feet, tip to body
vtail_sweep=35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-35.8                 //Feet,35.8 longitudinal distance from reference point, negative going aft
vtail_pos_vert=5.8                   //Feet, vertical distance from reference point, positive going up
elevator_area=70.5                  //Square feet
aileron_area=26.9                  //Square feet
rudder_area=56.2                  //Square feet
elevator_up_limit=22.5                  //Degrees
elevator_down_limit=19.5                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=20.0                  //Degrees
rudder_limit=26.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=172.0                 //Knots True (KTAS)
full_flaps_stall_speed=133.0                 //Knots True (KTAS)
cruise_speed=477 
max_indicated_speed=340.000000
max_mach=0.820020

[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

[fltsim.0]
title=AAV B752RR TURKMENISTAN AIRLINES
sim=aia_757_200_RR
model=RR
panel=
sound=RR
texture=turkmenistan
kb_checklists=
kb_reference=
atc_id=EZ-A014
atc_airline=TURKMENISTAN AIRLINES
atc_flight_number=701
ui_manufacturer=AI
ui_type=Boeing 757-200
ui_variation=Turkmenistan Airlines
description=AI Aardvark 757-200 (RR)
atc_id_color=0000000000
visual_damage=1
atc_heavy=1


[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
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