[fltsim.0]
title=FCB 9o9 Retro
sim=boeing747-400
model=
panel=
sound=
texture=retro
kb_checklists=
kb_reference=FCB9o9_ref
atc_id=F19A
atc_airline=FCB
atc_flight_number=CB399
atc_heavy=1
ui_manufacturer="FCB"
ui_type="9o9"
ui_variation="Retro"
ui_typerole="Commercial Airliner"
ui_createdby="Hoa Nguyen"
description="The FCB9o9 is a technologically advanced aircraft that can complete a trip half way around the world in one hour on autopilot (a few seconds in Warp mode). The aircraft is constructed with Intelligent Programmable Material which allows it to deform itself to the required shape on-demand."
[fltsim.1]
title=FCB 9o9 White
sim=boeing747-400
model=
panel=
sound=
texture=white
kb_checklists=
kb_reference=FCB9o9_ref
atc_id=F19B
atc_airline=FCB
atc_flight_number=CB400
atc_heavy=1
ui_manufacturer="FCB"
ui_type="9o9"
ui_variation="White"
ui_typerole="Commercial Airliner"
ui_createdby="Hoa Nguyen"
description="The FCB9o9 is a technologically advanced aircraft that can complete a trip half way around the world in one hour on autopilot (a few seconds in Warp mode). The aircraft is constructed with Intelligent Programmable Material which allows it to deform itself to the required shape on-demand."
[fltsim.2]
title=FCB 9o9 Chameleon
sim=boeing747-400
model=
panel=
sound=
texture=chameleon
kb_checklists=
kb_reference=FCB9o9_ref
atc_id=F19C
atc_airline=FCB
atc_flight_number=CB401
atc_heavy=1
ui_manufacturer="FCB"
ui_type="9o9"
ui_variation="Chameleon"
ui_typerole="Commercial Airliner"
ui_createdby="Hoa Nguyen"
description="The FCB9o9 is a technologically advanced aircraft that can complete a trip half way around the world in one hour on autopilot (a few seconds in Warp mode). The aircraft is constructed with Intelligent Programmable Material which allows it to deform itself to the required shape on-demand. This limited edition also has the ability to change its color."
[General]
atc_type=
atc_model=
editable=0
performance="Engines\nFCB9o9 Hybrid Turbine\/Rocket\n\nCruise Speed (conventional fuel)\n0.85 mach 565 mph 910 km\/h\n\nMaximum Speed (rocket fuel)\n123,290 knots 141,880 mph 228,333 km\/h\n\nMaximum Range (conventional fuel)\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude\n100,000,000 ft 18,939 mi 30,480 km\n\nConventional Fuel Capacity\n57,285 gal 216,840 L\n\nBasic Empty Weight\n394,088 lb 178,755 kg\n\nMax Gross Weight\n875,000 lb 396,893 kg\n\nLength\n89 ft, 7 in 27.3 m\n\nWingspan\n113 ft, 2 in 34.5 m\n\nHeight\n31 ft, 4 in 9.6 m"
Category = airplane
[CameraDefinition.0]
Title = "Right Side"
Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description = View of the right wing from behind
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz = 5.5, 0.75, -22.2
InitialPbh = 8, 0, 30
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.1]
Title = "Left Side"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing from behind
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz = -5.5, 0.75, -22.2
InitialPbh = 8, 0, 330
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[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 = 0.3
ShowWeather = Yes
InitialXyz = 0, -10, -18
InitialPbh = -30, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[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 = 0.7
ShowWeather = Yes
InitialXyz = 0, 9.0, -80.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.4]
Title = "Nose"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646d}
Description = Looking backward from the front of the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
ShowWeather = Yes
InitialXyz = 0, 5.0, 40.0
InitialPbh = 5, 0, 180
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.5]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 40.8, 2.4, -10.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.6]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -40.8, 2.4, -10.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.7]
Title = "Inside Forward"
Guid = {5c1df273-034b-4e7f-953a-9d5e36f1646c}
Description = Looking forward from inside the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
ShowWeather = Yes
InitialXyz = 0, -0.5, -19
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.8]
Title = "Inside Down"
Guid = {5c1df273-034b-4e7f-953a-9e5e36f1646c}
Description = Looking down from inside the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
ShowWeather = Yes
InitialXyz = 0, 0.2, -9.2
InitialPbh = 90, 0, 0
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[CameraDefinition.9]
Title = "Inside Back"
Guid = {5c1df273-034c-4e7f-953a-9d5e26f1646d}
Description = Looking backward from inside the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
ShowWeather = Yes
InitialXyz = 0, -0.5, 0.3
InitialPbh = 0, 0, 180
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = No
ClipMode = Minimum
xyzRate = 10
xyzAccelleratorTime = 0
PitchPanRate = 30
HeadingPanRate = 75
PanAcceleratorTime = 0
zoompanscalar = 1
[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 = 875000 // (pounds)
empty_weight = 394088 // (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 = 0.0, -83.5, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 0.0, -27.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 0.0, -65.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 0.0, -50.0, 0.0, 8.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 0.0, -91.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 0.0, -119.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 0.0, -160.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 0.0, -52.0, 0.0, -6.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 0.0, -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 = 13352310
empty_weight_pitch_MOI = 24223159
empty_weight_yaw_MOI = 39531785
empty_weight_coupled_MOI = 0
[gpws]
max_warning_height = -5000
[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 = 5825.0 //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 = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 112.0 //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 = 1.0
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 = -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, -36.2, 1600, 0, 0.0, 70.0, 0.5, 3.5, 0.900, 0.1, 0.1, 0, 420, 450
point.1 = 1, -114.0, -18.0, -36.5, 1600, 1, 0.0, 13.0, 0.5, 2.5, 0.900, 0.1, 0.1, 2, 420, 450
point.2 = 1, -114.0, 18.0, -36.5, 1600, 2, 0.0, 13.0, 0.5, 2.5, 0.900, 0.1, 0.1, 3, 420, 450
point.3 = 2, -120.5, -56.56, -4.20, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0
point.4 = 2, -120.5, 56.56, -4.20, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0
point.5 = 2, -79.20, 0.0, -1.9, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0
point.6 = 2, -169.2, 0.0, 15.75, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0
point.7 = 4, -25.0, -18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.8 = 4, -25.0, 18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.9 = 4, -114.0, -18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.10 = 4, -114.0, 18.0, -34.2, 2500, 0, 0.0, 0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.11 = 5, -114.0, 0.0, -34.2, 0, 0, 0.0, 20, 0.00, 0.0, 0.50, 0.0, 0.0, 0, 0, 0
static_pitch = 0.0
static_cg_height = 36.0
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 2 //Amphibian
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 = -83.5, 0, 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
Com.1 = 1, 0
Nav.1 = 1, 0, 1
[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_dummy
water=fx_dummy
waterspeed=fx_dummy
dirt=fx_dummy
concrete=fx_dummy
touchdown=fx_dummy
contrail=fx_dummy
startup=fx_dummy
vaportrail_l=fx_dummy
vaportrail_r=fx_dummy
l_wingtipvortice=fx_dummy
r_wingtipvortice=fx_dummy
EngineFire=fx_dummy
EngineDamage=fx_dummy
EngineOilLeak=fx_dummy
SkidPavement=fx_dummy
WheelSnowSpray=fx_dummy
WheelWetSpray=fx_dummy
WetEngineWash=fx_dummy
SnowEngineWash=fx_dummy
PistonFailure=fx_dummy
[exits]
number_of_exits = 1
exit.0 = 0.4, -100.0, -19.0, -18.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
