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CRJ-700 default aircraft.cfg help please


OperationNacho

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[fltsim.0]
title=Bombardier CRJ 700 Paint1
sim=Bombardier_CRJ_700
model=
panel=
sound=
texture=1
kb_checklists=BombardierCRJ700_check
kb_reference=BombardierCRJ700_ref
atc_id=NCRJ70
atc_parking_types=GATE,RAMP
atc_airline=Orbit
ui_manufacturer="Bombardier"
ui_type="CRJ700"
ui_variation="Orbit Airlines"
ui_typerole="Regional Jet"
ui_createdby="Microsoft Corporation"
description="The CRJ (Canadair Regional Jet) family of aircraft was derived from the Canadair Challenger business jet, which began its operational life as the LearStar 600. The Bombardier Canadair CRJ700, which entered service in 2001, is a stretched version of the CRJ100/200 regional jet, with increased seating capacity from 50 to 70. With increased length and upgraded landing gear, the CRJ700 features a longer wing span and leading edge slats. Like other members of the CRJ family, the CRJ700 features an electronic flight instrument system (EFIS) avionics suite and “glass cockpit” instrumentation."

[fltsim.1]
title=Bombardier CRJ 700 Paint2
sim=Bombardier_CRJ_700
model=
panel=
sound=
texture=2
kb_checklists=BombardierCRJ700_check
kb_reference=BombardierCRJ700_ref
atc_id=NCRJ70
atc_airline=Pacifica
atc_parking_types=GATE,RAMP
ui_manufacturer="Bombardier"
ui_type="CRJ700"
ui_variation="Pacifica Airlines"
ui_typerole="Regional Jet"
ui_createdby="Microsoft Corporation"
description="The CRJ (Canadair Regional Jet) family of aircraft was derived from the Canadair Challenger business jet, which began its operational life as the LearStar 600. The Bombardier Canadair CRJ700, which entered service in 2001, is a stretched version of the CRJ100/200 regional jet, with increased seating capacity from 50 to 70. With increased length and upgraded landing gear, the CRJ700 features a longer wing span and leading edge slats. Like other members of the CRJ family, the CRJ700 features an electronic flight instrument system (EFIS) avionics suite and “glass cockpit” instrumentation."

[fltsim.2]
title=Bombardier CRJ 700 Paint4
sim=Bombardier_CRJ_700
model=
panel=
sound=
texture=4
kb_checklists=BombardierCRJ700_check
kb_reference=BombardierCRJ700_ref
atc_id=NCRJ70
atc_parking_types=GATE,RAMP
ui_manufacturer="Bombardier"
ui_type="CRJ700"
ui_variation="Executive Jet"
ui_typerole="Regional Jet"
ui_createdby="Microsoft Corporation"
description="The CRJ (Canadair Regional Jet) family of aircraft was derived from the Canadair Challenger business jet, which began its operational life as the LearStar 600. The Bombardier Canadair CRJ700, which entered service in 2001, is a stretched version of the CRJ100/200 regional jet, with increased seating capacity from 50 to 70. With increased length and upgraded landing gear, the CRJ700 features a longer wing span and leading edge slats. Like other members of the CRJ family, the CRJ700 features an electronic flight instrument system (EFIS) avionics suite and “glass cockpit” instrumentation."

[fltsim.3]
title=Bombardier CRJ 700
sim=Bombardier_CRJ_700
model=
panel=
sound=
texture=
kb_checklists=BombardierCRJ700_check
kb_reference=BombardierCRJ700_ref
atc_id=NCRJ70
atc_parking_types=GATE,RAMP
ui_manufacturer="Bombardier"
ui_type="CRJ700"
ui_variation="White"
ui_typerole="Regional Jet"
ui_createdby="Microsoft Corporation"
description="The CRJ (Canadair Regional Jet) family of aircraft was derived from the Canadair Challenger business jet, which began its operational life as the LearStar 600. The Bombardier Canadair CRJ700, which entered service in 2001, is a stretched version of the CRJ100/200 regional jet, with increased seating capacity from 50 to 70. With increased length and upgraded landing gear, the CRJ700 features a longer wing span and leading edge slats. Like other members of the CRJ family, the CRJ700 features an electronic flight instrument system (EFIS) avionics suite and “glass cockpit” instrumentation."

[General]
atc_type=BOMBARDIER
atc_model=CRJ700
editable=0
performance="Cruise Speed\n0.78 Mach		515 mph	829 km\/h\n\nEngine options\nGeneral Electric CF34-8C1 turbofans 12,670 lb thrust\n\nMaximum Range\n1,702 nm		3,152 km\n\nService Ceiling\n41,000 ft		12,497 m\n\nFuel Capacity\n3,036 gal		11,488 L\n\nEmpty Weight\n43,200 lb		19,595 kg\n\nMaximum Gross Weight\n72,500 lb		32,885 kg\n\nLength\n106 ft, 8 in		32.5 m\n\nWingspan\n76 ft, 3 in		23.2 m\n\nHeight\n24 ft, 10 in		7.6 m\n\nSeating\n70\n\nUseful Load\n18,800 lb		8,527 kg"
Category = airplane

[CameraDefinition.0]
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 = .52
ShowWeather = Yes
InitialXyz = -2.2, -1.2, -7
InitialPbh = 0, 0, 13
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
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 = .75
ShowWeather = Yes
InitialXyz = 0, 3, -35.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
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 = 25.8, 1.6, 0.0
InitialPbh = 6, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
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 = -25.8, 1.6, 0.0
InitialPbh = 6, 0, 80
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 = 74945.0                      // (pounds)
empty_weight = 43500.0                          // (pounds)

reference_datum_position     =   49.7,  0, 0    // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -50.0,  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   = 413776
empty_weight_roll_MOI    = 188879
empty_weight_yaw_MOI     = 578254
empty_weight_coupled_MOI = 0.0


[airplane_geometry]
wing_area               = 738.7                 //Square feet
wing_span               = 76.25                 //Feet
wing_root_chord         = 17.3                  //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             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 8                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 20                                   // degrees
flaps-position.2 = 20                                   // degrees
flaps-position.3 = 25                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[flaps.1]
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 = 0                                    // degrees
flaps-position.2 = 8                                    // degrees
flaps-position.3 = 20                                   // degrees
flaps-position.4 = 30                                   // degrees
flaps-position.5 = 45                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -74.0, -7.5, 2.1                     //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -74.0,  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            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 12670                 //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   =  -52.7,  0.0, -4.0,  688.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  -54.3, -7.7, -3.5, 1118.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  -54.3,  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,  -8.50,  0.00,  -6.70, 1600, 0, 0.5625, 46.8, 0.80, 2.5, 0.55, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -56.50, -6.76,  -8.60, 1600, 1, 1.0,     0.0, 0.90, 2.5, 0.65,  9.0,  9.0, 2, 260.0, 260.0
point.2=1, -56.50,  6.76,  -8.60, 1600, 2, 1.0,     0.0, 0.90, 2.5, 0.65,  9.0,  9.0, 3, 260.0, 260.0
point.3=2, -65.00, -39.00,  0.00, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -65.00,  39.00,  0.00, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -43.00,   0.00, -3.80, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -98.00,   0.00, 16.00, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.7=2,  -8.00,   0.00, -2.00, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.8=2, -80.00,   0.00, -1.50, 1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

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 = -11.1, -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
light.0 = 3,  -64.70, -37.00,  -0.50, fx_navredm ,
light.1 = 3,  -64.70,  37.00,  -0.50, fx_navgrem ,
light.2 = 3,  -104.63,   0.00,  14.30, fx_navwhi ,
light.3 = 1,  -29.00,   0.00, -2.30, fx_beaconb ,
light.4 = 2,  -104.63,   0.00,  15.00, fx_strobe ,
light.5 = 1,  -32.50,   0.00,  7.00, fx_beaconh ,
light.6 = 4,  -10.00,   0.00,  3.90, fx_vclighth,
light.7 = 2,  -64.50, -36.50,  -0.50, fx_strobe ,
light.8 = 2,  -64.50,  36.50,  -0.50, fx_strobe ,


[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

Still thinking about a new flightsim only computer!  ✈️

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