[fltsim.0]
title=Airbus A340-313X Lufthansa Star Alliance
sim=TomA343
model=
panel=340
sound=
texture=dlh
kb_checklists=
kb_reference=
atc_id=D-CIAJ
atc_airline=Lufthansa
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Airbus
ui_type="A340-300"
ui_variation=Lufthansa Star Alliance
ui_typerole="Commercial Airliner"
ui_createdby="Thomas Ruth"
description="The Airbus A340 is a long-range, four-engine, wide-body commercial passenger jet airliner that was developed and produced by the European aerospace company Airbus. The A340 was assembled in Toulouse, France. It seats up to 375 passengers in the standard variants and 440 in the stretched -600 series."
[General]
atc_type=AIRBUS
atc_model=A343
editable=1
performance="Reisegeschwindigkeit\nMach 0.84 555 mph 893 kmh\n\nTriebwerkoption \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximale Reichweite \n5.960 nm 6.859 sm 11.038 km\n\nDienstgipfelhöhe \n42.000 Fuß 12.800 m\n\nTreibstoffmenge \n45.220 Gallonen 171.160 L \n\nMaximales Startgewicht \n660.000 lbs 299.370 kg\n\nLänge \n242 Fuß, 4 Zoll 73.9 m\n\nSpannweite \n199 Fuß, 11 Zoll 60.9 m\n\nHöhe \n60 Fuß, 8 Zoll 18.5 m\n\nSitzplätze \n386 bis 550 \n\nFrachtkapazität \n7.552 Kubikfuß 213.8 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, 1.183, -9.753
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, 1.183, -9.753
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=-1.914, 1.046, 26.133
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=1.914, 1.046, 26.133
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, -3.127, -19.004
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, -4.33, 26.056
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, 12.155, -33.902
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 = 606271 // (pounds)
empty_weight = 285000 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -12, 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 = "3740.0, -30.0, 0.0, 0.0, Sitz 1-16" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "2550.0, -72.5, 0.0, 0.0, Sitz 16-29" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "2000.0, 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 = -18.09, -64.14, -4.67 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 3.28, -30.96, -8.59 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 3.28, 30.96, -8.59 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -18.09, 64.14, -4.67 //(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 = 28.9 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 31230 //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, 66.95, 0.00, -16.53, 1181.1, 0, 4.521, 90.0, 1.00, 2.5, 0.7235, 4.0, 4.0, 0, 270.0, 270.0
point.1=1, -18.60, -17.60, -18.68, 1574.8, 1, 4.521, 0.0, 2.61, 1.6, 0.7470, 6.9, 6.9, 2, 270.0, 270.0
point.2=1, -18.60, 17.60, -18.68, 1574.8, 2, 4.521, 0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0
point.3=1, -18.60, 0.05, -18.68, 1574.8, 2, 4.521, 0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0
point.4=2, -43.97, -97.21, 4.80, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.5=2, -43.97, 97.21, 4.80, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.6=2, -107.2, 0.00, 2.53, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, 86.35, 0.00, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
//[contact_points]
//point.0=1, 66.95, 0.00, -16.43, 1181.1, 0, 4.521, 90.0, 1.00, 2.5, 0.7235, 4.0, 4.0, 0, 270.0, 270.0
//point.1=1, -18.60, -17.60, -18.38, 1574.8, 1, 4.521, 0.0, 2.61, 1.6, 0.7470, 6.9, 6.9, 2, 270.0, 270.0
//point.2=1, -18.60, 17.60, -18.38, 1574.8, 2, 4.521, 0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0
//point.3=1, -18.60, 0.05, -18.38, 1574.8, 2, 4.521, 0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0
//point.4=2, -43.97, -97.21, 4.80, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
//point.5=2, -43.97, 97.21, 4.80, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
//point.6=2, -107.2, 0.00, 2.53, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
//point.7=2, 86.35, 0.00, 0.00, 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 = 17.56
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]
normal_pressure = 3000.0 //PSI
electric_pumps = 1 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2
[Views]
//eyepoint = 69.66, -1.43, 3.65
eyepoint = 79.854, -1.76, 3.60
[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 = 240 // 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
[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, -22.38, 0.00, -10.70, fx_T332beacon ,
light.1 = 1, 17.22, 0.00, 9.74, fx_T332beacon ,
light.2 = 2,-118.31, 0.00, 6.60, fx_navwhih ,
light.3 = 3,-118.31, 0.00, 6.60, fx_navwhih ,
light.4 = 5, 26.04, 18.39, -3.28, fx_T332land ,
light.5 = 5, 26.04, -18.39, -3.28, fx_T332land ,
light.6 = 9,-103.26, 8.79, 20.02, fx_T332logo ,
light.7 = 9,-103.26, -8.79, 20.02, fx_T332logo ,
light.8 = 4, 79.14, 0.00, 4.56, fx_vclighth ,
//light.9 = 6, 22.64, 29.49, -8.18, fx_T332eng ,
//light.10 = 6, 22.64, -29.49, -8.18, fx_T332eng ,
//light.11 = 8, -15.35, 66.26, 2.70, fx_T332wing ,
//light.12 = 8, -15.35, -66.26, 2.70, fx_T332wing ,
[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, 107.30, -9.0, 0.88,0 //openclose rate percent
//per second, longitudinal, lateral, vertical positions from
//datum (feet), type (0=Main 1=Cargo 2=Emergency)
//number_of_exits = 4
exit.0 = 0.4, 68.87, -9.0, 5.5, 0 ;Percent per second
exit.1 = 0.04, -66.35, 7.497, -4.905, 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 = -10.5, 0.0, -8.2, 11188.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = -100.5, 0.0, 5.7, 1646.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -8.9, -27.9, -1.7, 11247.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -8.9, 27.9, -1.7, 11247.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -36.3, -67.9, 2.5, 964.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -36.3, 67.9, 2.5, 964.0, 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 = 3893.0 //Square feet
wing_span = 197.83 //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 = 1 //Are winglets available?
wing_sweep = 31.5 //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 = 583.0 //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 = 85.9 //Square feet
aileron_area = 48.0 //Square feet
rudder_area = 121.0 //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 = 482.0 //Knots True (KTAS)
max_mach = 0.86
max_indicated_speed = 340 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
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
