[fltsim.0]
title=Thai A300-600R
sim=TomA306
model=RPW
panel=306PW
sound=
texture=THAI
kb_checklists=
kb_reference=
atc_id=TSTAC
atc_airline=Thai
atc_flight_number=1124
atc_heavy=1
ui_manufacturer=Airbus
ui_typerole=Commercial Airliner
ui_createdby=Thomas Ruth
ui_type=A300-600R
ui_variation=Thai International

[fltsim.1]
title=American Airlines A300-600R
sim=TomA306
model=RGE
panel=306GE
sound=
texture=AA
kb_checklists=
kb_reference=
atc_id=N70074
atc_airline=American
atc_flight_number=1124
atc_heavy=1
ui_manufacturer=Airbus
ui_typerole=Commercial Airliner
ui_createdby=Thomas Ruth
ui_type=A300-600R
ui_variation=American Airlines

[General]
atc_type=AIRBUS
atc_model=A306
editable=1
performance="Reisegeschwindigkeit\nMach 0.78         515 mph         829 kmh\n\nTriebwerkoption        \nP&W 4158\CF6-80C2\n\nMaximale Reichweite              \n4.070 nm          7.540 km\n\nDienstgipfelhцhe    \n42.000 FuЯ           12.800 m\n\nTreibstoffmenge       \n18.000 Gallonen        68.150 L \n\nMaximales Startgewicht     \n375.100 lbs        170.500 kg\n\nLдnge    \n177 FuЯ, 3 Zoll         54.08 m\n\nSpannweite      \n147 FuЯ, 2 Zoll          44.85 m\n\nHцhe        \n54 FuЯ, 6 Zoll           16.62 m\n\nSitzplдtze       \nca 266 \n\nFrachtkapazitдt        \n147.4 Kubikmeter\n"
Category=airplane


[CameraDefinition.0]
Title=Left wingview
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Left trailing edge as seen from paxcabin
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=-3.318, 0.367, -5.665
InitialPbh=5, 0, 270
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Right wingview
Guid={D368D3EA-21FB-4d88-97BC-771106DCC59B}
Description=Right trailing edge as seen from paxcabin
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=3.318, 0.367, -5.665
InitialPbh=5, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Left engine view
Guid={E4F8DA49-C99E-40ae-8467-AC874BB497B6}
Description=Left engine as seen from flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=-2.514, 0.645, 12.536
InitialPbh=5, 0, 215
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Right engine view
Guid={C3CD1BAC-B511-4557-B3CE-C5F6EAD00807}
Description=Right engine as seen from flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=2.514, 0.645, 12.536
InitialPbh=5, 0, 145
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Main gear cam
Guid={D1EE9F66-E2A5-4dd8-9874-D87E96E1F980}
Description=Main gear as seen from the belly fairing
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=0, -3.23, -7.977
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.5]
Title=Nose gear cam
Guid={5D9AC711-EC3E-4e47-AF27-820DE14AF3E1}
Description=Runway as seen from the nose gear
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=0, -3.454, 17.314
InitialPbh=0, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.6]
Title=Tail cam
Guid={665E785E-73B0-44e7-89F6-229E1F6BA1C9}
Description=Aircraft as seen from the tip of the vertical stabilizer
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.3
ShowWeather=Yes
InitialXyz=0, 11.058, -26.887
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
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=.7
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.0, 0.0, 0.0
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title=Jump Seat
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.7
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.00, -1.2
InitialPbh=2, 0, 0

[WEIGHT_AND_BALANCE]
max_gross_weight = 378500                       // (pounds)
empty_weight = 200400                           // (pounds)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 =  "170.0,  86.0,  -2.0,    0.0, Pilot"                  //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 =  "170.0,  86.0,   2.0,    0.0, Kopilot"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =  "850.0,   0.0,   0.0,    0.0, Besatzung"                   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =  "850.0,  52.0,   0.0,    0.0, Erste Klasse"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "1870.0,  11.0,   0.0,    0.0, Businessklasse"         //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "2740.0, -30.0,   0.0,    0.0, Sitz 1-16"             //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "1550.0, -72.5,   0.0,    0.0, Sitz 16-29"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "1800.0,  47.0,   0.0,   -6.0, Fracht vorne"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 =  "500.0, -67.0,   0.0,   -6.0, Fracht hinten"              //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


;Moments of Inertia
empty_weight_pitch_MOI  = 7000000
empty_weight_roll_MOI   = 10500000
empty_weight_yaw_MOI    = 6300000
empty_weight_coupled_MOI= 0.0
CG_forward_limit = 0.000
CG_aft_limit = 1.000

[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 = 0.33, -25.98, -8.56                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 0.33,  25.98, -8.56                    //(feet) longitudinal, lateral, vertical distance from reference datum
//fuel_flow_scalar = 1.0      ORIGINAL
fuel_flow_scalar = 1.00                     //Scalar for fuel flow efficiency
min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature=-30       

[TurbineEngineData]
fuel_flow_gain = 0.002                          //Gain on fuel flow
inlet_area = 90.0                              //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 61500                           //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

[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)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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
light_logo         = 0, 5 , 17.0
light_wing         = 0, 5 , 17.0

        //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)

[contact_points]
point.0=1,  55.77,   0.00, -15.95, 1181.1, 0, 1.669, 90.0, 0.4921, 2.7667, 0.7235, 4.0, 4.0, 0, 270.0, 270.0
point.1=1,  -8.17, -14.73, -16.53, 1574.8, 1, 2.064,  0.0, 0.4921, 2.6401, 0.7470, 6.9, 6.9, 2, 270.0, 270.0
point.2=1,  -8.17,  14.73, -16.53, 1574.8, 2, 2.064,  0.0, 0.4921, 2.6401, 0.7470, 7.1, 7.1, 3, 270.0, 270.0
point.3=2, -26.30, -73.64,   2.89,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -26.30,  73.64,   2.89,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -96.67,   0.00,   6.18,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  79.24,   0.00,  -0.35,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

static_pitch = 0.10
static_cg_height = 17.00
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 = 1.0  //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  = 1         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[Views]
//eyepoint = 69.66, -1.43, 3.65
eyepoint = 68.89, -1.76, 3.60
//A300  = 69.90, -1.77, 3.77

[flaps.0]      //Trailing Edge
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.2                                  // 0.0 .. 1.0
extending-time   = 25                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 3                                    // degrees
flaps-position.2 = 15                                    // degrees
flaps-position.3 = 20                                   // degrees
flaps-position.4 = 26                                   // degrees
flaps-position.5 = 35                                   // degrees
damaging-speed   = 220                                  // KIAS
blowout-speed    = 260                                  // KIAS
lift_scalar           = 0.547 //0.57
drag_scalar           = 1.25
pitch_scalar          = 0
system_type           = 1                   //Hydraulic

[flaps.1]    //Leading Edge
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 23                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 18                                    // degrees
flaps-position.2 = 18                                    // degrees
flaps-position.3 = 22                                   // degrees
flaps-position.4 = 22                                   // degrees
flaps-position.5 = 27                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 270                                 // KIAS
lift_scalar           = 0.5 //0.55 
drag_scalar           = 0.4
pitch_scalar          = 0.2
system_type           = 1                   //Hydraulic

[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

[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

[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
direction_indicator.1=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]
max_pressure=5.15   // PSI
vacuum_type=2       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

[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

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing,6taxi,7reco,8wing,9logo,10cabin
light.0 = 1,  15.95,   0.00,  10.04, fx_T332beacon ,
light.1 = 1,   9.81,   0.00,  -9.22, fx_T332beacon ,
light.2 = 5,  11.13,  11.28,  -15.57, fx_T332land  ,
light.3 = 5,  11.13, -11.28,  -15.57, fx_T332land  ,
light.4 = 9, -85.01,   8.79,  20.82, fx_T332logo  ,
light.5 = 9, -85.01,  -8.79,  20.82, fx_T332logo  ,
light.6 = 10,  67.62,   0.00,   4.30, fx_vclighth  ,

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[exits]
number_of_exits = 4
exit.0 = 0.4,  58.57, -7.12, 2.8, 0    ;Percent per second
exit.1 = 0.04,   -46.13,  7.50, -5.59, 1    ;Percent per second
exit.2 = 0.4,   -28.803, -8.540, -3.868, 2    ;Percent per second
exit.3 = 0.4,   -28.803, -8.540, -3.868, 2    ;Percent per second

[fuel]
Center1   =  4.4,   0.0, -5.4, 4646.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2   =  -81.82,   0.0, 6.1, 1625.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = 2.99, -31.7,  0,  4639.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 2.99,  31.7,  0,  4639.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux  = -16.6, -57.6,  1.8,  1222.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -16.6,  57.6,  1.8,  1222.0, 3.0     //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               = 2893.0                //Square feet
wing_span               = 147.2                 //Feet
wing_root_chord         = 35.1                  //Feet
wing_dihedral           = 5.5                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.72                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 28.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 20.0                  //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              = 716.9                //Square feet
htail_span              = 63.16                  //Feet
htail_pos_lon           = -100.07                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 5.87                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 34.0                  //Degrees, horizontal tail leading edge
vtail_area              = 560.0                 //Square feet
vtail_span              = 30.84                  //Feet, tip to body
vtail_sweep             = 39.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -99.74                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 25.6                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 75.9                 //Square feet
aileron_area            = 48.0                  //Square feet
rudder_area             = 126.0                 //Square feet
elevator_up_limit       = 30.0                  //Degrees
elevator_down_limit     = 15.0                  //Degrees
aileron_up_limit        = 30.0                  //Degrees
aileron_down_limit      = 15.0                  //Degrees
rudder_limit            = 25.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
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
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
//fly_by_wire=1

[Reference Speeds]
flaps_up_stall_speed    = 150.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 120.0                 //Knots True (KTAS)
cruise_speed            = 447.0                 //Knots True (KTAS)
max_mach                = 0.82
max_indicated_speed     = 340                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1500.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 90
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=0.10
nav_proportional_control=11.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=19.0
gs_integrator_control=0.530
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0


[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

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9