[fltsim.0] title=Project Opensky - B737-700 Shanghai Airlines sim=OSBoeing737-700w model=we panel= sound= texture=shanghai kb_checklists=Boeing737-800_check kb_reference=Boeing737-800_ref atc_id=B-5260 atc_airline=Shanghai Air atc_flight_number=746 atc_heavy=0 atc_parking_types=GATE, RAMP, CARGO atc_parking_code=CSH ui_manufacturer=Boeing ui_type=737-700 ui_variation=Shanghai Airlines visual_damage=1 description=Project Opensky - Boeing 737-700\nVersion - Version 2004.9.3\n\nModel Designer\n Hiroshi Igami\n\nFlight Dynamics/Scenario/Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: \n 3,383 nautical miles [General] atc_type=BOEING atc_model=B737 editable=0 Category=airplane performance=Passengers\n2-class conf: 162\n\nCargo\nTotal lower hold volume: \n1,555 cu ft (44 cu m)\n\nDimensions\nSpan 117 ft 5 in (34.3 m)\nLength 129 ft 6 in (39.5 m)\nHeight 41 ft 2 in (12.5 m)\nEngines: GE CFM56-7B\nTO Thrust Rating: 27,300 lb (121 kN)\n\nMax Fuel Cap.: 6,875 US gal (26,035 L)\nMaxTOW: 174,200 lb\n\nTypical Cruise Speed\n @ FL350: M.785 [General] atc_type=BOEING atc_model=B737 editable=0 performance=Passengers\n2-class conf: 128\n\nCargo\nTotal lower hold volume: \n1,002 cu ft (28.4 cu m)\n\nDimensions\nSpan 117 ft 5 in (35.79 m)\nLength 129 ft 6 in (39.5 m)\nHeight 41 ft 2 in (12.5 m)\nEngines: GE CFM56-7B\nTO Thrust Rating: 27,300 lb (121 kN)\n\nMax Fuel Cap.: 6,875 US gal (26,035 L)\nMaxTOW: 174,200 lb\n\nTypical Cruise Speed\n @ FL350: M.785 Category = airplane [CameraDefinition.0] Title = "Right Side Window" Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description = View of the right wing from the passenger cabin Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 3.2, 1.8, -5 InitialPbh = 5, 0, 100 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Left Side Window" Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description = View of the left wing from the passenger cabin Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -3.2, 1.8, -5 InitialPbh = 5, 0, 260 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.2] Title = "Right Engine" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Right Engine View Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .50 ShowWeather = Yes InitialXyz = 1.0, 1.1, 3.4 InitialPbh = 5, 0, 41 // ^v <> XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.3] Title = "Left Engine" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = Left Engine View Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.50 ShowWeather = Yes InitialXyz = -1.0, 1.1, 3.4 InitialPbh = 5, 0, 319 // ^v <> XyzAdjust = TRUE Category=Aircraft MomentumEffect = No ClipMode=Minimum [CameraDefinition.4] Title = "Right Side" Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description = Right Outside Fuselage View Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .50 ShowWeather = Yes InitialXyz = 8.0, 0.0, 20 // <> ^v InitialPbh = 0, 0, 225 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.5] Title = "Left Side" Guid = {8ff6c134-098d-409f-baec-caba3f683f98} Description = Left Outside Fuselage View Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .50 ShowWeather = Yes InitialXyz = -8.0, 0.0, 20 // <> ^v InitialPbh = 0, 0, 135 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available [WEIGHT_AND_BALANCE] max_gross_weight = 155000.000 empty_weight = 83000.000 reference_datum_position = 5.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum // New FS-X Numbers max_number_of_stations = 50 station_load.0 = 170.0, 46.3, -1.5, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170.0, 46.3, 1.5, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 510.0, 0.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 1360.0, 33.4, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 5440.0, 16.1, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 5440.0, -9.7, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 4760.0, -28.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = 4000.0, 24.7, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = 1000.0, -34.4, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0 = "Pilot" station_name.1 = "Co-Pilot" station_name.2 = "Crew" station_name.3 = "First Class" station_name.4 = "Coach 3-10" station_name.5 = "Coach 11-18" station_name.6 = "Coach 19-25" station_name.7 = "Forward Baggage" station_name.8 = "Aft Baggage" ;Moments of Inertia empty_weight_pitch_MOI = 1600655 empty_weight_roll_MOI = 588050 empty_weight_yaw_MOI = 2148751 empty_weight_coupled_MOI = 0 //max_number_of_stations = 50 // New FS2004 Numbers // Max 2-class - 128, Max Econ only - 148 // Actual Total PAX - 38,150 lbs //station_load.0 = 1360.000000, 25.000000, 0.000000, 0.000000, 1st Class-8 //station_load.1 =20400.000000, 0.000000, 0.000000, 0.000000, Econ Class-120 // Total Opensky Cargo - 17,350 lbs //station_load.2 =2400.000000, 20.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd //station_load.3 =2400.000000, -51.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft //station_load.4 = 174.000000, -57.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk // Moments of Inertia //empty_weight_pitch_MOI = 1595057.280 //empty_weight_roll_MOI = 1649603.980 //empty_weight_yaw_MOI = 2742152.520 //empty_weight_coupled_MOI = 0.000 //CG_forward_limit= 0.000 //CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.201 induced_drag_scalar =1.201 elevator_effectiveness =1.500 aileron_effectiveness =0.350 rudder_effectiveness =0.251 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.751 aileron_trim_effectiveness =0.501 rudder_trim_effectiveness =0.501 [GeneralEngineData] engine_type = 1 Engine.0 = 4.750, -16.100, -4.500 Engine.1 = 4.750, 16.100, -4.500 fuel_flow_scalar = 1.30 min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] bypass_ratio = 5.1 fuel_flow_gain = 0.002 inlet_area = 20.270 rated_N2_rpm = 29920.000 static_thrust = 26000.000 afterburner_available = 0 reverser_available = 1.000 [jet_engine] thrust_scalar =1.000 [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, 5, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 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 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 [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) // // Nose Gear point.0 = 1, 32.200, -0.67, -8.26, 1181.1, 0, 1.777, 75.00, 0.350, 0.650, 0.850, 9.000, 9.000, 0, 235.0, 320.0 point.1 = 1, 32.200, 0.67, -8.26, 1181.1, 0, 1.777, 75.00, 0.350, 0.650, 0.850, 9.000, 9.000, 0, 235.0, 320.0 // Left Main Gear point.2=1, -5.00, -9.99, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0 point.3=1, -5.00, -7.16, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0 // Right Main Gear point.4=1, -5.00, 9.99, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0 point.5=1, -5.00, 7.16, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0 // // //======================================================================================================================================================= // //FUll Motion, Realistic feel, true footprint contact points // // Nose Gear //point.0 = 1, 32.200, -0.67, -10.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0 //point.1 = 1, 32.200, 0.67, -10.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0 // // Left Main Gear //point.2=1, -5.000, -9.99, -11.00, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0 //point.3=1, -5.000, -7.16, -11.00, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0 // // Right Main Gear //point.4=1, -5.000, 9.99, -11.00, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0 //point.5=1, -5.000, 7.16, -11.00, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0 // // // // Scrape Points // Fuselage point.6 = 2, 50.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Nose point.7 = 2, 44.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom fwd point.8 = 2, 0.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom center point.9 = 2, -17.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom aft point.10= 2, 38.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top fwd point.11= 2, 0.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top center point.12= 2, -35.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top aft point.13= 2, 38.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd lt point.14= 2, 38.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd rt point.15= 2, 0.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center lt point.16= 2, 0.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center rt point.17= 2, -35.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft left point.18= 2, -35.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft right point.19= 2, -42.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tailskid aft point.20= 2, -56.000, 0.000, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tail-APU // Tailplane, vert/horiz stabs point.21= 2, -53.000, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab fwd point.22= 2, -58.000, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab aft point.23= 2, -60.000, -23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Horizontal Stab aft lt point.24= 2, -60.000, 23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Horizontal Stab aft rt // Wings point.25= 2, -15.000, -58.750, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip fwd point.26= 2, -20.000, -58.750, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip aft point.27= 2, -15.000, 58.750, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip fwd point.28= 2, -20.000, 58.750, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip aft point.29= 2, -2.000, -37.000, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid fwd point.30= 2, -12.000, -37.000, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid aft point.31= 2, -2.000, 37.000, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid fwd point.32= 2, -12.000, 37.000, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid aft // Engines point.33= 2, 20.900, -15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd point.34= 2, 20.900, 15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd point.35= 2, 15.000, -15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom point.36= 2, 15.000, 15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine bottom max_number_of_points = 37 static_pitch= -1.000 //static_cg_height=7.67 static_cg_height=8.10 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 0 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.43 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=44.00, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum - Opensky Model //eyepoint=38.70, -1.31, 3.7 // Default FS VC [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, 6=taxi, 7=recognition, 8=wing, 9=logo light.1 = 1, 1.600, 0.000, -4.500, Opensky_beacon , light.2 = 1, 9.300, 0.400, 9.300, Opensky_beacon , light.3 = 4, 46.000, 0.000, 3.500, Opensky_Boeing_vclight , light.4 = 3, 20.000, 0.000, -3.000, Opensky_nacelle_refl , // front cargo light.5 = 3, -20.000, 0.000, -2.000, Opensky_nacelle_refl , // rear cargo light.6 = 3, 33.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door light.7 = 8, 14.000, -36.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights light.8 = 8, 14.000, 35.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights light.9 = 8, 25.400, -6.200, 2.100, Opensky_nav_yellow , // flap inspection light light.10= 8, 25.400, 6.200, 2.100, Opensky_nav_yellow , // flap inspection light light.11= 5, 30.000, -6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights light.12= 5, 30.000, 6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights light.13= 8, 23.000, -12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights light.14= 8, 23.000, 12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights light.15= 6, 43.750, 0.000, -12.550, Opensky-taxi-refl , // gear bay taxi light rays from taxi lights light.16= 3, -53.000, 0.000, 7.000, Opensky_nav_yellow , // Tail Nav Light light.17= 2, -53.000, 0.000, 7.000, fx_strobeh , // Tail Strobe Light [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 = 100, 200 aileron = 100, 200 rudder = 100, 200 [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 direction_indicator.1=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [vacuum_system] max_pressure=5.15 // PSI vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 //[exits] //number_of_exits = 3 //exit_rate.0 = 0.10, 36.6, -5.0, 3.0, 0 ;Percent per second //exit_rate.1 = 0.10, -38.5, 4.5, -3.0, 1 ;Percent per second //exit_rate.2 = 0.12, 33.5, 3.5, -4.0, 2 ;Percent per second [exits] number_of_exits = 3 exit.0 = 0.1, 36.6, -5.0, 3.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1 = 0.1, -38.5, 4.5, -3.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2 = 0.1, 33.5, 3.5, -4.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=Opensky_737NG_sparks, 1 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=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=30,25,20,15,10 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] // Total Fuel - 46,063 lbs, 6814 US Gallons -- Total Usable Fuel - 46,000 lbs, 6804 US Gallons // Center1 = 5.000, 0.000, 0.000, 4260.000, 0.000 // Center Tank LeftMain = 3.000, -19.000, 0.000, 1272.000, 0.000 // Main 1 Tank RightMain = 3.000, 19.000, 0.000, 1272.000, 0.000 // Main 2 Tank fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 1137.000 wing_span = 117.500 wing_root_chord = 18.000 wing_dihedral = 6.200 wing_incidence = 1.000 wing_twist = -0.500 oswald_efficiency_factor= 0.750 wing_winglets_flag = 0 wing_sweep = 25.000 wing_pos_apex_lon = 15.000 wing_pos_apex_vert = 0.000 htail_area = 338.000 htail_span = 41.700 htail_pos_lon = -35.000 htail_pos_vert = 0.000 htail_incidence = 0.000 htail_sweep = 30.000 vtail_area = 224.000 vtail_span = 20.000 vtail_sweep = 35.000 vtail_pos_lon = -47.000 vtail_pos_vert = 5.800 elevator_area = 70.500 aileron_area = 26.900 rudder_area = 56.200 elevator_up_limit = 24.000 elevator_down_limit = 18.000 aileron_up_limit = 25.000 aileron_down_limit = 15.000 rudder_limit = 15.000 elevator_trim_limit = 15.000 spoiler_limit = 30.000 spoilerons_available = 1 aileron_to_spoileron_gain = 2.000 min_ailerons_for_spoilerons=15.000 min_flaps_for_spoilerons = 0.000 auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 142.000 full_flaps_stall_speed = 113.000 cruise_speed = 452.160 max_mach = 0.82 max_indicated_speed = 340 //Red line (KIAS) [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 [stall_warning] type=2 stick_shaker=1 [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.3 // 0.0 .. 1.0 extending-time = 36 // 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 = 1.00 drag_scalar = 0.40 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Inboard Leading Edge Flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.3 // 0.0 .. 1.0 extending-time = 36 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 20 // degrees flaps-position.2 = 20 // degrees flaps-position.3 = 20 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 20 // degrees flaps-position.6 = 20 // degrees flaps-position.7 = 20 // degrees flaps-position.8 = 20 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.00 drag_scalar = 0.15 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 36 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 10 // degrees flaps-position.2 = 10 // degrees flaps-position.3 = 10 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 20 // degrees flaps-position.6 = 20 // degrees flaps-position.7 = 20 // degrees flaps-position.8 = 20 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.00 drag_scalar = 0.15 pitch_scalar= 1.0 system_type = 1 //Hydraulic [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [altimeters] altimeter.0=1 altimeter.1=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots