[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 [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 [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 ; [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 [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 [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 sim=aia_757_200_RR model=RR panel= sound=RR texture=turkmenistan kb_checklists= kb_reference= atc_id=EZ-A014 atc_airline=TURKMENISTAN atc_flight_number=245 ui_manufacturer=AI Aardvark ui_type=Boeing 757-200 ui_variation=Turkmenistan description=AI Aardvark 757-200 (RR) atc_id_color=0000000000 visual_damage=0 atc_heavy=1
