[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
