[fltsim.0] title=Bombardier Global Express 9H-FED sim=GEX_FSX model= panel= sound= texture=9H-FED kb_checklists= kb_reference= atc_id=9H-FED atc_parking_types=GATE,RAMP atc_airline= ui_manufacturer="Bombardier" ui_type="Global Express" ui_variation="9H-FED" ui_typerole="Regional Jet" ui_createdby="IRIS Flight Simulation Software" description="" [General] atc_type=BOMBARDIER atc_model=CRJ700 editable=0 performance="" Category = airplane [CameraDefinition.0] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 0.8, 1.1, -4.0 InitialPbh = 10, 0, 90 XyzAdjust = TRUE Category=Aircraft MomentumEffect = FALSE ClipMode=Minimum [CameraDefinition.1] Title = "Left Wing" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -0.8, 1.1, -4.0 InitialPbh = 10, 0, 270 XyzAdjust = TRUE Category=Aircraft MomentumEffect = No ClipMode=Minimum [CameraDefinition.001] Title = "Right Seat" Guid = {8ff6c134-098d-409f-baec-caba3f683f98} Origin = Virtual Cockpit MomentumEffect = YES SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = .6 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=1.1, 0.0, 0.0 InitialPbh=2, 0, 0 [CameraDefinition.002] Title = "Center Console" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.8 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.54, 0.3, -0.05 InitialPbh=75, 0, 0 [CameraDefinition.003] Title = "Engine Controls" Guid = {a5741a54-ea6d-4580-9709-c99161e38a83} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.54, 0.0, 0.28 InitialPbh=65.0, 0, 0 [CameraDefinition.004] Title = "Overhead Panel" Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 SmoothZoomTime = 2.0 ZoomPanScalar = 1.15 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.55, -0.58, -0.3 InitialPbh=-49.7, 0, 0 [WEIGHT_AND_BALANCE] max_gross_weight = 80500.0 // (pounds) empty_weight = 47250.0 // (pounds) reference_datum_position = 55.35, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position = -56.0, 0, 7 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -8.67, -1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, -8.67, 1.4, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 11000, -62.0, 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 = "Passengers" ;Moments of Inertia empty_weight_pitch_MOI = 363576 empty_weight_roll_MOI = 188879 empty_weight_yaw_MOI = 578254 empty_weight_coupled_MOI = 0.0 [airplane_geometry] wing_area = 760.0 //Square feet wing_span = 81.5 //Feet wing_root_chord = 18.9 //Feet wing_dihedral = 0.0 //Degrees wing_incidence = 1.5 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 27.0 //Degrees, wing leading edge wing_pos_apex_lon = -42.2 //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 = 192.0 //Square feet htail_span = 14.4 //Feet htail_pos_lon = -95.9 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 12.7 //Feet, vertical distance from reference point, positive going up htail_incidence = 4.0 //Degrees htail_sweep = 35.0 //Degrees, horizontal tail leading edge vtail_area = 108.0 //Square feet vtail_span = 11.6 //Feet, tip to body vtail_sweep = 44.0 //Degrees, vertical tail leading edge vtail_pos_lon = -86.7 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.7 //Feet, vertical distance from reference point, positive going up elevator_area = 42.1 //Square feet aileron_area = 22.0 //Square feet rudder_area = 21.4 //Square feet elevator_up_limit = 28.0 //Degrees elevator_down_limit = 20.0 //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 spoiler_extension_time = 2.0 //Seconds spoilerons_available = 1 //Spoilerons Available? aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain min_ailerons_for_spoilerons = 5 //Degrees min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate auto_spoiler_available = 1 positive_g_limit_flaps_up = 3.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up = -2.0 //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 = 112.0 //Knots True (KTAS) full_flaps_stall_speed = 102.0 //Knots True (KTAS) cruise_speed = 473.0 //Knots True (KTAS) max_mach = 0.83 max_indicated_speed = 335.0 //Red line (KIAS) [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 [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 flaps-position.1 = 8 // degrees flaps-position.2 = 20 // degrees flaps-position.3 = 30 // degrees flaps-position.4 = 45 // degrees damaging-speed = 250 // KIAS blowout-speed = 280 // KIAS [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -83.7, -7.5, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -83.7, 7.5, 2.1 //(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 = 0.0025 //Gain on fuel flow inlet_area = 9.4 //Square Feet, engine nacelle inlet area rated_N2_rpm = 17710 //RPM, second stage compressor rated value static_thrust = 13123 //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 [fuel] Center1 = -55.2, 0.0, -4.0, 688.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -59.4, -7.7, -3.5, 1118.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -59.4, 7.7, -3.5, 1118.0, 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 //0 Class //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 [contact_points] point.0=1, -23.63, 0.00, -7.0, 1600, 0, 0.5625, 46.8, 0.28, 1.11, 0.20, 10.0, 10.0, 0, 260.0, 260.0 point.1=1, -63.43, -6.76, -8.3, 1600, 1, 1.0, 0.0, 1.2, 1.25, 0.20, 9.0, 9.0, 2, 260.0, 260.0 point.2=1, -63.43, 6.76, -8.3, 1600, 2, 1.0, 0.0, 1.2, 1.25, 0.20, 9.0, 9.0, 3, 260.0, 260.0 static_pitch = -1.8 static_cg_height = 7.3 gear_system_type=1 //Hydraulic emergency_extension_type=2 //None=0,Pump=1,Gravity=2 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.2 //Brake scalar auto_brakes = 0 hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 30.0 max_generator_alternator_amps = 400.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 5 , 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 2 , 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 1 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [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 [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 [stall_warning] type=2 stick_shaker=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 2 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 turn_indicator.1=0,0 [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 Adf.2 = 1 Transponder.1 = 1 Marker.1 = 1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 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=30,15 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [Views] eyepoint = -16.73, -1.65, 4.28 [exits] number_of_exits = 3 exit.0 = 0.4, -16.90, -4.5, 3.9, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1 = 0.4, -74.00, -4.5, 0.5, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2 = 0.4, -16.50, 4.5, 0.5, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing ref: 55.35 [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_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [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