[fltsim.0]
title=Boeing 747SCA
sim=747_SCA
model=
panel=
sound=
texture=
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N905NA
atc_airline=Boeing
atc_flight_number=1223
atc_heavy=1
ui_manufacturer="Boeing"
ui_type="747SCA"
ui_variation="Shuttle Carrier"
ui_typerole="Special Airliner"
ui_createdby="Microsoft Corporation"
description="This is one of the two 747 that the NASA uses to ferry the Space Shuttle. Note the operating restrictions on speed and altitude."




[General]
atc_type=BOEING
atc_model=B744
editable=0
performance="Cruise Speed\n0.6 Mach\/250 KTS unconditional     \n\nEngine \nPratt & Whitney JT9D-7\n\nMaximum Range mated\/unmated\n1,000 nm\/5,000 nm \n\nMaximum Certified Operating Altitude mated\/unmated\n15,000 ft\/26,000ft \n\nFuel Capacity\n47,210 gal\n\nBasic Empty Weight\n318,053 lb  \nMax Gross Taxi Weight\n713,000 lb\nMax Gross Brake Release Weight\n710,000 lb\nMax Gross Landing Weight\n600,000 lb\n\nMinimum Temperature at Altitude\n15 degrees (F) (-9 degrees C) \n\nLength\n231 ft, 10 in\n\nWingspan\n195 ft, 8 in\n\nHeight\n63 ft, 5 in\n\nSeating\nNone\n\nCrew\n2 Pilots 1\/2 Flight Engineer unmated\/mated\n\nCopyright 2008 things-to-come
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 = 1.0
ShowWeather = Yes
InitialXyz = 5.5, 0.75, -13
InitialPbh = 0, 0, 95
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 = 1.0
ShowWeather = Yes
InitialXyz = -5.5, 0.75, -13
InitialPbh = 0, 0, 265
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[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 = .58
ShowWeather = Yes
InitialXyz = -11, -4.1, -16
InitialPbh = 0, 0, 44
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[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 = .75
ShowWeather = Yes
InitialXyz = 0, 9.0, -80.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
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 = 40.8, 1.4, 4.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.5]
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 = -40.8, 1.4, 4.0
InitialPbh = 6, 0, 90
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 = .75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.25, 0.0, 0.0
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title = "Radio Stack"
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 = .75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.30, -0.05
InitialPbh=85, 0, 0

[CameraDefinition.003]
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 = 0.8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.635, -0.58, -0.2
InitialPbh=-55.0, 0, 0

[CameraDefinition.004]
Title = "Engine Controls"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
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=0.6, 0.3, 0
InitialPbh=59.5, 0, 0


[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 = 775000                       // (pounds)
empty_weight = 318053                          // (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  =  1700.0,	 -83.5,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3  =  5440.0,	 -27.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4  =  5780.0,	 -65.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5  =  7140.0,	 -50.0,	 0.0,	 8.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6  = 10710.0,	 -91.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7  = 18020.0,	-119.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8  = 23800.0,	-160.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.9  = 18000.0,	 -52.0,	 0.0,	-6.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.10 =  6000.0,	-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    = 22352310
empty_weight_pitch_MOI   = 40223159
empty_weight_yaw_MOI     = 72531785
empty_weight_coupled_MOI = 0


[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               = 6225.0                //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    = 147.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 118.0                 //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   = 1.7
induced_drag_scalar    = 1.1
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, -17.2, 1600, 0, 2.0, 70.0, 0.5, 3.5, 0.900,  9.0,  8.0, 0, 220, 250
point.1 = 1, -114.0,   -18.0, -20.0, 1600, 1, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0,  9.0, 2, 220, 250
point.2 = 1, -114.0,    18.0, -20.0, 1600, 2, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0,  9.0, 3, 220, 250
point.3 = 2, -152.6,  -103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
point.4 = 2, -152.6,   103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
point.5 = 2,    3.0,     0.0,   0.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
point.6 = 2, -222.7,     0.0,   4.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
                                     
static_pitch = 0.0
static_cg_height = 17.0
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //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 = 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 = -18.55, -2.0, 11.0              ; 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
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                   
light.1 = 3, -223.85,    0.00,   8.85, fx_navwhih ,
light.2 = 2, -228.97,    0.00,  44.62, fx_strobeh ,
light.3 = 1,  -45.05,    0.00,  15.65, fx_beaconh ,
light.4 = 1,  -80.22,    0.00, -11.05, fx_beaconb ,
light.5 = 4,  -18.24,    0.00,  11.19, fx_vclighth,

[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_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[exits]
number_of_exits = 2
exit.0 = 0.4, -30.30,  -9.0,  0.88,0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -146.0,   8.0, -7.5, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, -42.30,   9.0, -7,   2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

[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

[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots