[fltsim.0]
title=Project Opensky - Boeing 737-700 Cargo Dreamliner with Virtual Cockpit
sim=OSBoeing737-700C
model=vc
panel=
sound=
texture=boeing
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=N737C
atc_airline=EXPERIMENTAL
atc_flight_number=1
atc_heavy=0
atc_parking_types=RAMP
atc_parking_code=
ui_manufacturer=Project Opensky
ui_type=737-600C VC
ui_variation=Boeing Dreamliner with Virtual Cockpit
visual_damage=1
description=Project Opensky - Boeing 737-600 Cargo\nCargo Mode\nVersion - Version 2004.9.3\n\nModel Designer\n Hiroshi Igami, Giles Hacon, Felipe Falanghe\n\nFlight Dynamics/Scenario/Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Tom Harlaar\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: \n 3,383 nautical miles\n\nBoeing textures: \n AJ Nikoley \n\ The 737-700C (Convertible) is the first member of the Boeing Next-Generation 737 family to be offered in both an all-passenger and all-cargo layout. The 737-700C highlights the outstanding flexibility of the 737 family. The 737-700C was launched Sept. 3, 1997, when the U.S. Naval Reserve ordered two. The Naval Reserve calls the model the C-40 Clipper. The 737-700C is the first new all-cargo 737 Boeing has developed since 1966, when the 737-200 Convertible was launched. The 737-700C, also available with a Quick Change option, allows airlines to alternate between passenger and cargo layouts on a daily, weekly or seasonal basis depending on market requirements. The 737-600 Convertible with the Quick Change option incorporates palletized seating to enable the airplane to be converted from passenger to freighter and freighter to passenger configurations in less than one hour.
[General]
atc_type=BOEING
atc_model=B737
editable=0
performance=Passengers\nCargo Mode\nTotal Main Deck hold volume:\n3,520 cu ft (99.7 cu m) \n\nTotal lower hold volume: \n1,002 cu ft (28.4 cu m)\n\nDimensions\nSpan 112 ft 7 in (34.3 m)\nLength 129 ft 6 in (39.5 m)\nHeight 41 ft 2 in (12.5 m)\nEngines: GE CFM56-7B24\nTO Thrust Rating: 24,000 lb\n\nMax Fuel Cap.: 6,875 US gal (26,035 L)\nMaxTOW: 174,200 lb\n\nTypical Cruise Speed\n @ FL350: M.785
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 = 0.4
ShowWeather = Yes
InitialXyz = 0.2, 1.2, -1.7
InitialPbh = 5, 0, 80
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 = 0.4
ShowWeather = Yes
InitialXyz = -0.2, 1.2, -2.2
InitialPbh = 5, 0, 280
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 = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.94, 0.0, 0.0
InitialPbh=2, 0, 0
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
max_gross_weight = 171000.000
empty_weight = 84580.000
reference_datum_position = 5.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170.0, 46.3, -1.5, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170.0, 46.3, 1.5, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 510.0, 0.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 1360.0, 33.4, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 5440.0, 16.1, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 5440.0, -9.7, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 4760.0, -28.0, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 4000.0, 24.7, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 1000.0, -34.4, 0.0, 0.0 //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 = "Coach 3-10"
station_name.5 = "Coach 11-18"
station_name.6 = "Coach 19-25"
station_name.7 = "Forward Baggage"
station_name.8 = "Aft Baggage"
// Moments of Inertia
empty_weight_pitch_MOI = 1595057.280
empty_weight_roll_MOI = 1649603.980
empty_weight_yaw_MOI = 2742152.520
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.201
induced_drag_scalar =1.201
elevator_effectiveness =1.500
aileron_effectiveness =0.350
rudder_effectiveness =0.251
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.751
aileron_trim_effectiveness =0.501
rudder_trim_effectiveness =0.501
[GeneralEngineData]
engine_type = 1
Engine.0 = 4.750, -16.100, -4.500
Engine.1 = 4.750, 16.100, -4.500
fuel_flow_scalar = 1.30
min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear
[TurbineEngineData]
bypass_ratio = 5.1
fuel_flow_gain = 0.002
inlet_area = 20.270
rated_N2_rpm = 29920.000
static_thrust = 24000.000
afterburner_available = 0
reverser_available = 1.000
[jet_engine]
thrust_scalar =1.000
[electrical]
;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
[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)
//
// Nose Gear
point.0 = 1, 32.200, -0.67, -8.26, 1181.1, 0, 1.777, 75.00, 0.350, 0.650, 0.850, 9.000, 9.000, 0, 235.0, 320.0
point.1 = 1, 32.200, 0.67, -8.26, 1181.1, 0, 1.777, 75.00, 0.350, 0.650, 0.850, 9.000, 9.000, 0, 235.0, 320.0
// Left Main Gear
point.2=1, -5.00, -9.99, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0
point.3=1, -5.00, -7.16, -9.20, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.650, 6.9, 6.9, 2, 230.0, 320.0
// Right Main Gear
point.4=1, -5.00, 9.99, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0
point.5=1, -5.00, 7.16, -9.20, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.650, 7.1, 7.1, 3, 230.0, 320.0
//
//
//=======================================================================================================================================================
//
//FUll Motion, Realistic feel, true footprint contact points
//
// Nose Gear
//point.0 = 1, 32.200, -0.67, -10.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//point.1 = 1, 32.200, 0.67, -10.85, 1181.1, 0, 1.777, 75.00, 3.000, 1.500, 0.650, 9.000, 9.000, 0, 235.0, 320.0
//
// Left Main Gear
//point.2=1, -5.000, -9.99, -11.00, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//point.3=1, -5.000, -7.16, -11.00, 1574.8, 1, 1.442, 0.00, 3.000, 2.000, 0.650, 6.900, 6.900, 2, 230.0, 320.0
//
// Right Main Gear
//point.4=1, -5.000, 9.99, -11.00, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//point.5=1, -5.000, 7.16, -11.00, 1574.8, 2, 1.442, 0.00, 3.000, 2.000, 0.650, 8.100, 7.100, 3, 230.0, 320.0
//
//
//
// Scrape Points
// Fuselage
point.6 = 2, 50.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Nose
point.7 = 2, 44.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom fwd
point.8 = 2, 0.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom center
point.9 = 2, -17.000, 0.000, -3.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage bottom aft
point.10= 2, 38.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top fwd
point.11= 2, 0.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top center
point.12= 2, -35.000, 0.000, 16.800, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage top aft
point.13= 2, 38.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd lt
point.14= 2, 38.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width fwd rt
point.15= 2, 0.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center lt
point.16= 2, 0.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width center rt
point.17= 2, -35.000, -6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft left
point.18= 2, -35.000, 6.170, 1.500, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Fuselage width aft right
point.19= 2, -42.000, 0.000, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tailskid aft
point.20= 2, -56.000, 0.000, 10.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4, 0.000, 0.000 // Tail-APU
// Tailplane, vert/horiz stabs
point.21= 2, -53.000, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab fwd
point.22= 2, -58.000, 0.000, 31.750, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7, 0.000, 0.000 // Vertical stab aft
point.23= 2, -60.000, -23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Horizontal Stab aft lt
point.24= 2, -60.000, 23.550, 17.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Horizontal Stab aft rt
// Wings
point.25= 2, -15.000, -56.350, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip fwd
point.26= 2, -20.000, -56.350, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wingtip aft
point.27= 2, -15.000, 56.350, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip fwd
point.28= 2, -20.000, 56.350, 3.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wingtip aft
point.29= 2, -2.000, -37.000, 1.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid fwd
point.30= 2, -12.000, -37.000, 1.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5, 0.000, 0.000 // Left wing-mid aft
point.31= 2, -2.000, 37.000, 1.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid fwd
point.32= 2, -12.000, 37.000, 1.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6, 0.000, 0.000 // Right wing-mid aft
// Engines
point.33= 2, 20.900, -15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine fwd
point.34= 2, 20.900, 15.830, 0.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine fwd
point.35= 2, 15.000, -15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Left engine bottom
point.36= 2, 15.000, 15.830, -6.000, 787.400, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8, 0.000, 0.000 // Right engine bottom
max_number_of_points = 37
static_pitch= -1.000
//static_cg_height=7.67
static_cg_height=8.10
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 0 //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 = 0.43 //Brake scalar
auto_brakes=4
[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=55.20, -1.31, 3.7 //(feet) longitudinal, lateral, vertical distance from reference datum - Opensky Model
//eyepoint=38.70, -1.31, 3.7 // Default FS VC
[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, 6=taxi, 7=recognition, 8=wing, 9=logo
light.1 = 1, 1.600, 0.000, -4.500, Opensky_beacon ,
light.2 = 1, 9.300, 0.400, 9.300, Opensky_beacon ,
light.3 = 4, 55.400, 0.000, 1.900, fx_vclight ,
light.4 = 3, 20.000, 0.000, -3.000, Opensky_nacelle_refl , // front cargo
light.5 = 3, -20.000, 0.000, -2.000, Opensky_nacelle_refl , // rear cargo
light.6 = 3, 33.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door
light.7 = 8, 14.000, -36.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.8 = 8, 14.000, 35.000, 5.000, Opensky_wing_light , // wing/LE slat rays from inspection lights
light.9 = 8, 25.400, -6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.10= 8, 25.400, 6.200, 2.100, Opensky_nav_yellow , // flap inspection light
light.11= 5, 30.000, -6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.12= 5, 30.000, 6.200, -1.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.13= 8, 23.000, -12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.14= 8, 23.000, 12.500, -2.000, Opensky_nacelle_refl , // wing/LE slat rays from inspection lights
light.15= 6, 43.750, 0.000, -12.550, Opensky-taxi-refl , // gear bay taxi light rays from taxi lights
light.16= 3, -53.000, 0.000, 7.000, Opensky_nav_yellow , // Tail Nav Light
light.17= 2, -53.000, 0.000, 7.000, fx_strobeh , // Tail Strobe Light
[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 = 100, 200
aileron = 100, 200
rudder = 100, 200
[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 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 4
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.12 ;Percent per second
exit_rate.2 = 0.12 ;Percent per second
exit_rate.3 = 0.12 ;Percent per second
[folding_wings]
wing_fold_system_type=4 ;0=None
fold_rates=0.12,0.11 ;Percent per second
TailHook] // shift+C For opening cargo door.
tailhook_length=4 ;(feet)
tailhook_position = -10.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
Read more: http://flyawaysimulation.com/postt28208.html#ixzz0fqUJbM5Z
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=Opensky_737NG_sparks, 1
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=0.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=96.8
pitch_takeoff_ga= 0.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=32.000000
max_bank_acceleration=1.200000
max_bank_velocity=1.500000
max_throttle_rate=0.02800
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[fuel]
// Total Fuel - 46,063 lbs, 6814 US Gallons -- Total Usable Fuel - 46,000 lbs, 6804 US Gallons
//
Center1 = 5.000, 0.000, 0.000, 4260.000, 0.000 // Center Tank
LeftMain = 3.000, -19.000, 0.000, 1272.000, 0.000 // Main 1 Tank
RightMain = 3.000, 19.000, 0.000, 1272.000, 0.000 // Main 2 Tank
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 1137.000
wing_span = 112.700
wing_root_chord = 18.000
wing_dihedral = 6.200
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 25.000
wing_pos_apex_lon = 15.000
wing_pos_apex_vert = 0.000
htail_area = 338.000
htail_span = 41.700
htail_pos_lon = -35.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 224.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -47.000
vtail_pos_vert = 5.800
elevator_area = 70.500
aileron_area = 26.900
rudder_area = 56.200
elevator_up_limit = 24.000
elevator_down_limit = 18.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 15.000
elevator_trim_limit = 15.000
spoiler_limit = 30.000
spoilerons_available = 1
aileron_to_spoileron_gain = 2.000
min_ailerons_for_spoilerons=15.000
min_flaps_for_spoilerons = 0.000
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
[Reference Speeds]
flaps_up_stall_speed = 142.000
full_flaps_stall_speed = 113.000
cruise_speed = 452.160
max_mach = 0.82
max_indicated_speed = 340 //Red line (KIAS)
[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
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 15 // degrees
flaps-position.6 = 25 // degrees
flaps-position.7 = 30 // degrees
flaps-position.8 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.40
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.3 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 20 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 20 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 20 // degrees
flaps-position.6 = 20 // degrees
flaps-position.7 = 20 // degrees
flaps-position.8 = 20 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.7 // 0.0 .. 1.0
extending-time = 36 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 10 // degrees
flaps-position.3 = 10 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 20 // degrees
flaps-position.6 = 20 // degrees
flaps-position.7 = 20 // degrees
flaps-position.8 = 20 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.00
drag_scalar = 0.15
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
