[fltsim.0] title=FCB 9o9 Retro sim=boeing747-400 model= panel= sound= texture=retro kb_checklists= kb_reference=FCB9o9_ref atc_id=F19A atc_airline=FCB atc_flight_number=CB399 atc_heavy=1 ui_manufacturer="FCB" ui_type="9o9" ui_variation="Retro" ui_typerole="Commercial Airliner" ui_createdby="Hoa Nguyen" description="The FCB9o9 is a technologically advanced aircraft that can complete a trip half way around the world in one hour on autopilot. The aircraft is constructed with Intelligent Programmable Material which allows it to deform itself to the required shape on-demand." [fltsim.1] title=FCB 9o9 White sim=boeing747-400 model= panel= sound= texture=white kb_checklists= kb_reference=FCB9o9_ref atc_id=F19B atc_airline=FCB atc_flight_number=CB400 atc_heavy=1 ui_manufacturer="FCB" ui_type="9o9" ui_variation="White" ui_typerole="Commercial Airliner" ui_createdby="Hoa Nguyen" description="The FCB9o9 is a technologically advanced aircraft that can complete a trip half way around the world in one hour on autopilot. The aircraft is constructed with Intelligent Programmable Material which allows it to deform itself to the required shape on-demand." [General] atc_type=FCB atc_model=9o9 editable=0 performance="Engines\nFCB9o9 Hybrid Turbine\/Rocket\n\nCruise Speed (conventional fuel)\n0.85 mach 565 mph 910 km\/h\n\nMaximum Speed (rocket fuel)\n123,290 knots 141,880 mph 228,333 km\/h\n\nMaximum Range (conventional fuel)\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude\n100,000,000 ft 18,939 mi 30,480 km\n\nConventional Fuel Capacity\n57,285 gal 216,840 L\n\nBasic Empty Weight\n394,088 lb 178,755 kg\n\nMax Gross Weight\n875,000 lb 396,893 kg\n\nLength\n89 ft, 7 in 27.3 m\n\nWingspan\n113 ft, 2 in 34.5 m\n\nHeight\n31 ft, 4 in 9.6 m" Category = airplane [CameraDefinition.0] Title = "Right Side" Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description = View of the right wing from behind Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.6 ShowWeather = Yes InitialXyz = 5.5, 0.75, -22.2 InitialPbh = 8, 0, 30 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.1] Title = "Left Side" Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description = View of the left wing from behind Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.6 ShowWeather = Yes InitialXyz = -5.5, 0.75, -22.2 InitialPbh = 8, 0, 330 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.2] Title = "Landing Gear" Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description = View of the landing gear and left wing inboard flaps Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.3 ShowWeather = Yes InitialXyz = 0, -10, -18 InitialPbh = -30, 0, 0 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.3] Title = "Tail" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.7 ShowWeather = Yes InitialXyz = 0, 9.0, -80.0 InitialPbh = 5, 0, 0 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.4] Title = "Nose" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646d} Description = Looking backward from the front of the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.7 ShowWeather = Yes InitialXyz = 0, 5.0, 40.0 InitialPbh = 5, 0, 180 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.5] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 40.8, 2.4, -10.0 InitialPbh = 6, 0, 270 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.6] Title = "Left Wing" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = View from the left wing tip Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -40.8, 2.4, -10.0 InitialPbh = 6, 0, 90 XyzAdjust = TRUE Category=Aircraft MomentumEffect = No ClipMode=Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.7] Title = "Inside Forward" Guid = {5c1df273-034b-4e7f-953a-9d5e36f1646c} Description = Looking forward from inside the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.4 ShowWeather = Yes InitialXyz = 0, -0.5, -19 InitialPbh = 0, 0, 0 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.8] Title = "Inside Down" Guid = {5c1df273-034b-4e7f-953a-9e5e36f1646c} Description = Looking down from inside the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.3 ShowWeather = Yes InitialXyz = 0, 0.2, -9.2 InitialPbh = 90, 0, 0 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [CameraDefinition.9] Title = "Inside Back" Guid = {5c1df273-034c-4e7f-953a-9d5e26f1646d} Description = Looking backward from inside the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.4 ShowWeather = Yes InitialXyz = 0, -0.5, 0.3 InitialPbh = 0, 0, 180 XyzAdjust = TRUE Category = Aircraft MomentumEffect = No ClipMode = Minimum xyzRate = 10 xyzAccelleratorTime = 0 PitchPanRate = 30 HeadingPanRate = 75 PanAcceleratorTime = 0 zoompanscalar = 1 [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 = 875000 // (pounds) empty_weight = 394088 // (pounds) reference_datum_position = 83.5, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -90.5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170.0, -19.0, -2.0, 8.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170.0, -19.0, 2.0, 8.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 0.0, -83.5, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 0.0, -27.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 0.0, -65.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 0.0, -50.0, 0.0, 8.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 0.0, -91.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = 0.0, -119.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = 0.0, -160.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9 = 0.0, -52.0, 0.0, -6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10 = 0.0, -123.0, 0.0, -6.0 //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 = "Business Class" station_name.5 = "Upper Deck" station_name.6 = "Coach 1-7" station_name.7 = "Coach 8-18" station_name.8 = "Coach 19-34" station_name.9 = "Forward Baggage" station_name.10 = "Aft Baggage" ;Moments of Inertia empty_weight_roll_MOI = 13352310 empty_weight_pitch_MOI = 24223159 empty_weight_yaw_MOI = 39531785 empty_weight_coupled_MOI = 0 [gpws] max_warning_height = -5000 [fuel] LeftMain = -96.0, -28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -96.0, 28.0, -4.0, 12546.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -112.0, -36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -112.0, 36.5, -3.0, 4482.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftTip = -130.0, -73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightTip = -130.0, 73.0, 0.0, 1322.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1 = -83.5, 0.0, -7.0, 17164.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2 = -193.5, 0.0, 6.0, 3300.0, 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=1 fuel_dump_rate = 0.0167 //Percent of max quantity per second, i.e. about 1 minute for full fuel [airplane_geometry] wing_area = 5825.0 //Square feet wing_span = 211.4 //Feet wing_root_chord = 48.8 //Feet wing_dihedral = 7.0 //Degrees wing_incidence = 2.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 37.5 //Degrees, wing leading edge wing_pos_apex_lon = -58.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = -5 //Feet, vertical distance from reference point, positive going up htail_area = 1470 //Square feet htail_span = 72.8 //Feet htail_pos_lon = -210.0 //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 = 0.0 //Degrees htail_sweep = 37.5 //Degrees, horizontal tail leading edge vtail_area = 1060 //Square feet vtail_span = 37.1 //Feet, tip to body vtail_sweep = 45.0 //Degrees, vertical tail leading edge vtail_pos_lon = -198.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 26.1 //Feet, vertical distance from reference point, positive going up elevator_area = 327 //Square feet aileron_area = 225 //Square feet rudder_area = 230 //Square feet elevator_up_limit = 25 //Degrees elevator_down_limit = 15 //Degrees aileron_up_limit = 25 //Degrees aileron_down_limit = 15 //Degrees rudder_limit = 31.5 //Degrees elevator_trim_limit = 20 //Degrees spoiler_limit = 45 //Degrees spoiler_extension_time = 2.0 //Seconds 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 auto_spoiler_available = 1 positive_g_limit_flaps_up = 4.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down= 3.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up = -3.0 //Design G load tolerance (negative, flaps up) negative_g_limit_flaps_down= -2.0 //Design G load tolerance (negative, flaps down) load_safety_factor = 1.5 //Design G load safety factor [Reference Speeds] flaps_up_stall_speed = 140.0 //Knots True (KTAS) full_flaps_stall_speed = 112.0 //Knots True (KTAS) cruise_speed = 505.0 //Knots True (KTAS) max_mach = 0.92 max_indicated_speed = 365.0 //Red line (KIAS) [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 10 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.7 drag_scalar = 0.9 pitch_scalar= 0.9 system_type = 1 //Hydraulic [flaps.1] type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1.0 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.3 drag_scalar = 0.1 pitch_scalar= 0.1 system_type = 1 //Hydraulic [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 = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -107.5, -69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = -76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = -107.5, 69.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 60.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 56750 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? ThrustSpecificFuelConsumption = 0.40 [jet_engine] thrust_scalar = 1.0 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1800.0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_max_rpm = 99 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=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.05 nav_proportional_control=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control = 18.0 gs_integrator_control = 0.33 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.0 [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, -25.0, 0.0, -36.2, 1600, 0, 36.0892, 70.0, 0.5, 3.5, 0.900, 9.0, 8.0, 0, 220, 250 point.1 = 1, -114.0, -18.0, -36.5, 1600, 1, 36.0892, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 2, 220, 250 point.2 = 1, -114.0, 18.0, -36.5, 1600, 2, 36.0892, 13.0, 0.5, 2.5, 0.900, 11.0, 9.0, 3, 220, 250 point.3 = 2, -120.5, -56.56, -1.97, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.4 = 2, -120.5, 56.56, -1.97, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.5 = 2, -79.20, 0.0, -1.9, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.6 = 2, -123.1, 0.0, -4.6, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.7 = 2, -169.2, 0.0, 15.75, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.8= 4, -25.0, -18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0 point.9= 4, -25.0, 18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0 point.10= 4, -114.0, -18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0 point.11= 4, -114.0, 18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0 point.12= 5, -114.0, 0.0, -34.2, 0, 0, 0.0, 20, 0.00, 0.0, 0.50, 0.0, 0.0, 0, 0, 0 static_pitch = 0.0 static_cg_height = 36.0 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 2 //Amphibian 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 = 1.24 //Brake scalar auto_brakes = 4 hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,1,1 //pumps on Eng1,2,3,4 [Views] eyepoint = -83.5, 0, 0 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [Radios] // Radio Type = availiable, standby frequency, has glide slope Com.1 = 1, 0 Nav.1 = 1, 0, 1 [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 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 2 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [vacuum_system] //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi max_pressure=5.150000 vacuum_type=2 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [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 [EFFECTS] wake=fx_dummy water=fx_dummy waterspeed=fx_dummy dirt=fx_dummy concrete=fx_dummy touchdown=fx_dummy contrail=fx_dummy startup=fx_dummy vaportrail_l=fx_dummy vaportrail_r=fx_dummy l_wingtipvortice=fx_dummy r_wingtipvortice=fx_dummy EngineFire=fx_dummy EngineDamage=fx_dummy EngineOilLeak=fx_dummy SkidPavement=fx_dummy WheelSnowSpray=fx_dummy WheelWetSpray=fx_dummy WetEngineWash=fx_dummy SnowEngineWash=fx_dummy PistonFailure=fx_dummy [exits] number_of_exits = 1 exit.0 = 0.4, -100.0, -19.0, -18.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [stall_warning] type=2 stick_shaker=0 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots