[fltsim.0]
title=Sludge FX F/A-18A 416 FLTS/NASA
sim=FA-18
model=
panel=
sound=
texture=416FLTS-NASA
kb_checklists=boeing_FA18_check
kb_reference=boeing_FA18_ref
atc_id=CS202
atc_airline=Air Force
atc_flight_number=CS202
ui_manufacturer="Sludge"
ui_type="FX F/A-18A"
ui_variation="416-FLTS/NASA"
ui_typerole="Experimental Jet"
ui_createdby="Microsoft Corporation"
description="The Hornet combines the ruggedness required of carrier-borne aircraft with speed and superior agility, especially at high angles of attack. Its powerful engines, canted vertical stabilizers, horizontal stabilators, large leading- and trailing-edge flaps, and sophisticated flight control system all contribute to a level of performance that makes the Hornet a versatile front-line fighter in several air forces around the world."
[fltsim.1]
title=Sludge FX F/A-18A VFC-12
sim=FA-18
model=
panel=
sound=
texture=VFC-12
kb_checklists=boeing_FA18_check
kb_reference=boeing_FA18_ref
atc_id=CS202
atc_airline=NAVY
atc_flight_number=CS202
ui_manufacturer="Sludge"
ui_type="FX F/A-18A"
ui_variation="VFC-12"
ui_typerole="Carrier-Based Fighter/Attack Jet"
ui_createdby="Microsoft Corporation"
description="The Hornet combines the ruggedness required of carrier-borne aircraft with speed and superior agility, especially at high angles of attack. Its powerful engines, canted vertical stabilizers, horizontal stabilators, large leading- and trailing-edge flaps, and sophisticated flight control system all contribute to a level of performance that makes the Hornet a versatile front-line fighter in several air forces around the world."
[fltsim.2]
title=Sludge FX F/A-18A VFA-132
sim=FA-18
model=
panel=
sound=
texture=VFA-132
kb_checklists=boeing_FA18_check
kb_reference=boeing_FA18_ref
atc_id=CS202
atc_airline=NAVY
atc_flight_number=CS202
ui_manufacturer="Sludge"
ui_type="FX F/A-18A"
ui_variation="VFA-132"
ui_typerole="Carrier-Based Fighter/Attack Jet"
ui_createdby="Microsoft Corporation"
description="The Hornet combines the ruggedness required of carrier-borne aircraft with speed and superior agility, especially at high angles of attack. Its powerful engines, canted vertical stabilizers, horizontal stabilators, large leading- and trailing-edge flaps, and sophisticated flight control system all contribute to a level of performance that makes the Hornet a versatile front-line fighter in several air forces around the world."
[fltsim.3]
title=Sludge FX F/A-18A VMFA-314
sim=FA-18
model=
panel=
sound=
texture=VMFA-314
kb_checklists=boeing_FA18_check
kb_reference=boeing_FA18_ref
atc_id=CS202
atc_airline=MARINE
atc_flight_number=CS202
ui_manufacturer="Sludge"
ui_type="FX F/A-18A"
ui_variation="VMFA-314"
ui_typerole="Carrier-Based Fighter/Attack Jet"
ui_createdby="Microsoft Corporation"
description="The Hornet combines the ruggedness required of carrier-borne aircraft with speed and superior agility, especially at high angles of attack. Its powerful engines, canted vertical stabilizers, horizontal stabilators, large leading- and trailing-edge flaps, and sophisticated flight control system all contribute to a level of performance that makes the Hornet a versatile front-line fighter in several air forces around the world."
[fltsim.4]
title=Sludge FX F/A-18A VMFA-323
sim=FA-18
model=
panel=
sound=
texture=VMFA-323
kb_checklists=boeing_FA18_check
kb_reference=boeing_FA18_ref
atc_id=CS202
atc_airline=MARINE
atc_flight_number=CS202
ui_manufacturer="Sludge"
ui_type="FX F/A-18A"
ui_variation="VMFA-323"
ui_typerole="Carrier-Based Fighter/Attack Jet"
ui_createdby="repaint by Ray Gagnon"
description="The Hornet combines the ruggedness required of carrier-borne aircraft with speed and superior agility, especially at high angles of attack. Its powerful engines, canted vertical stabilizers, horizontal stabilators, large leading- and trailing-edge flaps, and sophisticated flight control system all contribute to a level of performance that makes the Hornet a versatile front-line fighter in several air forces around the world."
[General]
atc_type=BOEING
atc_model=F18
editable=0
performance="Maximum Speed (high altitude)\t\n1.8 Mach 1,911 km\/h\n\nMaximum Speed (low altitude)\t\n720 kts 1,335 km\/h\n\nCruise Speed\t\n580 kts 1,074 km\/h\n\nEngines\t\n2 General Electric turbines, 6-stage afterburners\n\nEmpty Weight\t\n24,500 lb 11,113 kg\n\nMaximum Gross Weight\t\n56,000 lb 25,401 kg\n\nTakeoff Gross Weight\t\n37,000 16,783 kg\n\nLength\t\n56 ft 17 m\n\nWingspan\t\n37.4 ft 11.4 m\n\nHeight\t\n15.1 ft 4.60 m\n\nSeating\t\n1"
Category = airplane
[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
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, 1.3, -24.0
InitialPbh = 3, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {E095506E-D7E4-4d4e-B5D2-923B4F9D08FF}
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 = 20.0, 0.0, -2.0
InitialPbh = 0, 0, 275
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {4B6E64F5-D9E2-4f08-9295-BBD59B9F9B56}
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 = -20.0, 0.0, -2.0
InitialPbh = 0, 0, 80
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.3]
Title = "Nose"
Guid = {3D31E848-6F6F-45d4-8E43-6290708756E3}
Description =Looking back from the nose toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 2.0, 14.0
InitialPbh = 0, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.4]
Title = "Nose Gear"
Guid = {5517F522-6C47-40da-BE66-3D7E10520D75}
Description =Looking back from the nose gear
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, -0.9, 7.0
InitialPbh = 0, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.001]
Title = "Radio Stack"
Guid = {18EF1F08-7138-4530-948C-07698E51940D}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, -0.12, 0.0
InitialPbh=16.0, 0, 0
[CameraDefinition.002]
Title = "Left Side Panel"
Guid = {98AA4524-EE82-4035-9D2C-D9A8C7D82DBF}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.25, -0.05, -0.1
InitialPbh=36.0, 0, 300
[CameraDefinition.003]
Title = "Right Side Panel"
Guid = {765CCF83-D7CD-4486-8983-A5714310CDD5}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.25, -0.05, -0.1
InitialPbh=36.0, 0, 60
[WEIGHT_AND_BALANCE]
max_gross_weight = 56000.0 // (pounds), default fsx = 56000.0
empty_weight = 24500.0 // (pounds), default fsx = 24500.0
;Moments of Inertia
empty_weight_pitch_MOI = 62300
empty_weight_roll_MOI = 16645
empty_weight_yaw_MOI = 71170
empty_weight_coupled_MOI = 0.0
reference_datum_position = 29.00, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -34.20, 0, -0.6 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 800, -16.0, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_load.1=190.0, -34.0, -19.0, 3.0, AIM9
station_load.2=250.0, -33.0, -4.0, -1.0, AIM7
station_load.3=250.0, -33.0, 4.0, -1.0, AIM7
station_load.4=190.0, -34.0, 19.0, 3.0, AIM9
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.3 // slow down Hornet at high speeds
induced_drag_scalar = 1.2 // higher AoA drag, more realistic for CVN Ops
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 0.90
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 = -35.8, -2.5, -0.1 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -35.8, 2.5, -0.1 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = 0.01 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 4.2895 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 11000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 6 //Afterburner stages available?
afterburner_throttle_threshold = 0.85 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.81 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 1.74 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 1.0
//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=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]
;Gear
point.0=1, -18.00, 0.00, -6.475, 3600, 0, 1.0349, 75.0, 0.2300, 2.6, 0.9100, 3.0, 3.0, 0, 0.0, 0.0
point.1=1, -35.80, -8.00, -7.175, 3600, 1, 1.2349, 0.0, 1.1500, 1.2, 0.8456, 3.9, 3.9, 2, 0.0, 0.0
point.2=1, -35.80, 8.00, -7.175, 3600, 2, 1.2349, 0.0, 1.1500, 1.2, 0.8456, 3.7, 3.7, 3, 0.0, 0.0
//point.0=1, -18.00, 0.00, -6.70, 3600, 0, 1.0349, 75.0, 0.2300, 2.8, 0.9100, 3.0, 3.0, 0, 0.0, 0.0
//point.1=1, -35.80, -8.00, -7.10, 3600, 1, 1.2349, 0.0, 1.1500, 1.1, 0.8456, 3.9, 3.9, 2, 0.0, 0.0
//point.2=1, -35.80, 8.00, -7.10, 3600, 2, 1.2349, 0.0, 1.1500, 1.1, 0.8456, 3.7, 3.7, 3, 0.0, 0.0
;Wingtips
point.3=2, -37.83, -20.00, 0.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -37.83, 20.00, 0.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -5.00, 0.00, -1.50, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -50.00, -4.00, -2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -50.00, 4.00, -2.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -15.00, 0.00, 5.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -48.00, -6.60, 9.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-48.00, 6.60, 9.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
static_pitch = -0.10
static_cg_height = 7.0
gear_system_type=1 //Hydraulic
emergency_extension_type=2 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 0 //Normal
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
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 = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -17.0, 0.0, 3.5
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -26.70, -4.00, 1.40, fx_navredm,
light.1 = 3, -26.70, 4.00, 1.40, fx_navgrem,
light.2 = 3, -49.40, 5.80, 8.50, fx_navwhi,
light.3 = 1, -46.15, 5.81, 7.50, fx_beacon_sml,
light.4 = 1, -46.15, -5.81, 7.50, fx_beacon_sml,
light.5 = 10, -15.00, 0.00, 2.00, fx_vclight,
light.6 = 5, -17.10, 0.00, -2.00, fx_landing_light_Dante_sm,// fx_siroccogtx2_reflectors
light.7 = 5, -11.00, 0.00, -3.50, fx_fuselage_light_Dante,
light.8 = 8, -14.00, 0.00, 1.10, fx_F18_NoseVapor, //Wing Vortex Vapor
light.9 = 9, -17.20, -0.50, -2.45, fx_AOA_amber, // logo light
light.10= 6, -17.20, -0.50, -2.20, fx_AOA_green, // taxi light
light.11= 7, -17.20, -0.50, -2.70, fx_AOA_red, // recognition light
[flaps.0]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 2.05 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 12 // degrees
flaps-position.2 = 33 // degrees
maneuvering_flaps=0 //0=manual,1=auto
[flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 2.05 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 30 // degrees
flaps-position.2 = 45 // degrees
maneuvering_flaps=0 //0=manual, 1=auto
[Radios]
// Radio Type = available, 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
[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
[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
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[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
[EFFECTS]
//wake=fx_wake
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m, 1
EngineFire=fx_engfire_f18
vaportrail_l=fx_vaportrail_l
vaportrail_r=fx_vaportrail_r
//SkidPavement=fx_skidmark
[fuel]
LeftAux = -24.5, 0.0, 2.5, 418, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -27.0, 0.0, 2.5, 263, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//Center1 = -33.0, 0.0, -4.0, 380, 0.0 ;Center //Center Tank
RightMain = -32.0, 0.0, 2.5, 206, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -36.5, 0.0, 2.0, 532, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip = -35.3, -5.5, 1.0, 85, 0.0 ;Left Wing //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip = -35.3, 5.5, 1.0, 85, 0.0 ;Right Wing //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 = 0.00185 //Percent of max quantity per second
[airplane_geometry]
wing_area = 400.0 //Square feet
wing_span = 37.4 //Feet
wing_root_chord = 13.3 //Feet
wing_dihedral = 2.5 //Degrees
wing_incidence = -3.0 //Degrees
wing_twist = -1.5 //Degrees
oswald_efficiency_factor= 0.80 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //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 = 88.26 //Square feet
htail_span = 21.6 //Feet
htail_pos_lon = -47.6 //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 = 42.8 //Degrees, horizontal tail leading edge
vtail_area = 1050 //Square feet
vtail_span = 7.8 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -42.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 27.0 //Square feet
aileron_area = 13.5 //Square feet
rudder_area = 27.3 //Square feet
elevator_up_limit = 17.0 //Degrees
elevator_down_limit = 15.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 2.4 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 0 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 7.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 7.5 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -5.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -5.0 //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 = 580.0 //Knots True (KTAS)
max_mach = 1.7
max_indicated_speed = 999 //Red line (KIAS)
[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=27,14
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
[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
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[folding_wings]
wing_fold_system_type=1 // Available
fold_rates = 0.25,0.25 // Left,Right: 1/sec
[GPWS]
max_warning_height = -1
[VoiceAlerts]
//LowFuelPct = .188, -1, 60 // Low Fuel limit (percent), check BELOW, check every 60 seconds
OverGLimit = 7.5, 1, 1 // High G limit, check ABOVE, check every 1 seconds
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[tailhook]
cable_force_adjust = 0.65
[SMOKESYSTEM]
smoke.0=-62.50, 2.0, 0, fx_EG_Smoke_fa18
smoke.1=-62.50, -2.0, 0, fx_EG_Smoke_fa18