[fltsim.0]
title=Project Opensky - CaribCay PJ-BGI
sim=OSBoeing737-800w
model=W
panel=
sound=
texture=BGI
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=PJ-BGI
atc_airline=Cayman
atc_flight_number=1024
atc_heavy=0
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=BOE
ui_manufacturer=Boeing
ui_type=CaribCay B738/w
ui_variation=CaribCay PJ-BGI
visual_damage=1
description=Project Opensky - Boeing 737-800\nVersion - Version 2004.9.2\n\nModel Designer\n   Hiroshi Igami\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

[fltsim.1]
title=Project Opensky - CaribCay PJ-POS
sim=OSBoeing737-800w
model=W
panel=
sound=
texture=POS
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=PJ-POS
atc_airline=Cayman
atc_flight_number=1024
atc_heavy=0
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=BOE
ui_manufacturer=Boeing
ui_type=CaribCay B738/w
ui_variation=CaribCay PJ-POS
visual_damage=1
description=Project Opensky - Boeing 737-800\nVersion - Version 2004.9.2\n\nModel Designer\n   Hiroshi Igami\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

[fltsim.2]
title=Project Opensky - CaribCay PJ-SMX
sim=OSBoeing737-800w
model=W
panel=
sound=
texture=SMX
kb_checklists=Boeing737-800_check
kb_reference=Boeing737-800_ref
atc_id=PJ-SMX
atc_airline=Cayman
atc_flight_number=1024
atc_heavy=0
atc_parking_types=GATE, RAMP, CARGO
atc_parking_code=BOE
ui_manufacturer=Boeing
ui_type=CaribCay B738/w
ui_variation=CaribCay PJ-SMX
visual_damage=1
description=Project Opensky - Boeing 737-800\nVersion - Version 2004.9.2\n\nModel Designer\n   Hiroshi Igami\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


[General]
atc_type=BOEING
atc_model=B738
editable=0

performance=Passengers\n2-class conf: 162\n\nCargo\nTotal lower hold volume: \n1,555 cu ft (44 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 CFM56-7B\nTO Thrust Rating: 27,300 lb (121 kN)\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 = "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 = .52
ShowWeather = Yes
InitialXyz = -3.3, -1.8, -07
InitialPbh = 0, 0, 17
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
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 = .75
ShowWeather = Yes
InitialXyz = 0, 6.5, -55.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
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 = 30.8, 1.6, 4.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
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 = -30.8, 1.6, 4.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.4]
Title = "Starboard Wing Inboard Edge 30"
Guid = {E6F09AF1-BE8D-45b9-A321-E6070D456328}
Description = View over the starboard wing from passenger pov
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz =  1.5, 1.1, -3
InitialPbh = 10, 0, 100
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.5]
Title = "Port Wing Inboard Edge 30"
Guid = {283902FC-DE04-4ca4-A455-6A6B42ACA4D1}
Description = View over the port wing from passenger pov
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz = -1.5, 1.1, -3 
InitialPbh = 10, 0, 260
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.6]
Title = "Starboard Wing Inboard Edge 40"
Guid = {84AE889D-10E9-435f-8FA2-33FADE170A5F}
Description = View behind starboard trailing edge flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz =  1.5, 1.1, -9.8
InitialPbh = 5, 0, 60
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.7]
Title = "Port Wing Inboard Edge 40"
Guid = {3971E217-9966-466f-8A0A-A7A15C4AF102}
Description = View behind port trailing edge flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz =  -1.5, 1.1, -9.8
InitialPbh = 5, 0, 300
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum


[CameraDefinition.8]
Title = "Starboard Wing Inboard Edge 16"
Guid = {905DF62B-DFA4-4a29-9D93-6291438F3A32}
Description = View of starboard engine inlet leading edge and inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz =  1.5, 1.1, 6.0
InitialPbh = 10, 0, 130
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.9]
Title = "Port Wing Inboard Edge 16"
Guid = {F505C2C2-85E7-4f49-96F6-5D921103F566}
Description = View of port engine inlet leading edge and inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz =  -1.5, 1.1, 6.0
InitialPbh = 10, 0, 230
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum



[CameraDefinition.10]
Title = "Forward Airstairs"
Guid = {0783D08E-C927-45cb-9F9E-E676FB9FC48E}
Description = Walk round inspection start position
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .6
ShowWeather = Yes
InitialXyz = -6.0, -1.3, 10.43
InitialPbh = -8, 0, 60
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum




[CameraDefinition.11]
Title = "Main Landing Gear View"
Guid = {1B1771BD-C708-4df0-A12A-1B1AE86B8341}
Description = Eye Level Port Side Main Landing Gear
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = -10.0, -2.3, -12.0
InitialPbh = -5, 0, 25
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.12]
Title = "Fin Wide Camera - Fixed"
Guid = {01834B40-1CBF-42e5-9090-C5D916D90C53}
Description = Tailfin above static wicks
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = FALSE
InitialZoom = .6
ShowWeather = Yes
InitialXyz = 0.0, 9.3, -19.43
InitialPbh = 15, 0, 0
XyzAdjust = FALSE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum


[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 = 174700.000
empty_weight = 91300.000

reference_datum_position     =  5.000, 0.000, 0.000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  7.000, 0.000, 0.000 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

// New FS2004 Numbers
// Max 2-class - 160, Max Econ only - 184

// Actual Total PAX  - 38,150 lbs
station_load.0 = 2720.000000, 25.000000, 0.000000, 0.000000, 1st Class-16
station_load.1 =24140.000000,  0.000000, 0.000000, 0.000000, Econ Class-142

// Total Opensky Cargo - 17,350 lbs
station_load.2 =5925.000000,  20.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd 
station_load.3 =5925.000000, -61.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft 
station_load.4 = 174.000000, -67.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"

// 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 =1.000	//1.500
aileron_effectiveness  =1.000	//0.350
rudder_effectiveness   =0.751
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 = 1.2105
min_throttle_limit = -0.35                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[SMOKESYSTEM]
smoke.0 = -18.530,  5.350,   -17.200,    Opensky_revspray
smoke.1 = -18.530,  5.350,    17.200,    Opensky_revspray 


[TurbineEngineData]
bypass_ratio =  5.1
fuel_flow_gain = 0.002
inlet_area = 20.270
rated_N2_rpm = 29920.000
static_thrust = 27300                           //Lbs, Per GE
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,  48.450,  -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,  48.450,   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,  48.450,  -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,  48.450,   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,  64.000,  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,  54.000,  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, -25.000,  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, -45.000,  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, -60.900,  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, -57.600,   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, -62.600,   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, -65.650, -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, -65.650,  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, -58.750, 10.000,  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, -58.750, 10.000,  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,  58.750, 10.000,  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,  58.750, 10.000,  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,  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 wing-mid fwd
//point.30= 2, -12.000, -37.000,  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 wing-mid aft
//point.31= 2,  -2.000,  37.000,  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 wing-mid fwd
//point.32= 2, -12.000,  37.000,  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 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 Contact Points (3 point)

point.0 = 1,  49.350,   0.00, -8.26, 1181.1, 0, 1.777, 75.00, 0.350, 0.650, 0.850, 9.0, 9.0, 0, 235.0, 320.0 // tweaked CP
point.1 = 1,  -2.250, -11.00, -9.60, 1574.8, 1, 1.442,  0.00, 1.200, 1.200, 0.650, 6.9, 6.9, 2, 230.0, 320.0 // tweaked CP
point.2 = 1,  -2.250,  11.00, -9.60, 1574.8, 2, 1.442,  0.00, 1.200, 1.200, 0.650, 7.1, 7.1, 3, 230.0, 320.0 // tweaked CP

// Scrape Points
// Fuselage
point.3 = 2,  64.000,  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.4 = 2,  54.000,  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.5 = 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.6 = 2, -25.000,  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.7= 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.8= 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.9= 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.10= 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.11= 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.12= 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.13= 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.14= 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.15= 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.16= 2, -45.000,  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.17= 2, -60.900,  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.18= 2, -57.600,   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.19= 2, -62.600,   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.20= 2, -65.650, -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.21= 2, -65.650,  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.22= 2, -15.000, -58.750, 10.000,  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.23= 2, -20.000, -58.750, 10.000,  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.24= 2, -15.000,  58.750, 10.000,  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.25= 2, -20.000,  58.750, 10.000,  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.26= 2,  -2.000, -37.000,  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 wing-mid fwd
point.27= 2, -12.000, -37.000,  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 wing-mid aft
point.28= 2,  -2.000,  37.000,  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 wing-mid fwd
point.29= 2, -12.000,  37.000,  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 wing-mid aft

// Engines
point.30= 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.31= 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.32= 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.33= 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 = 34

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 = 0.72   //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=55.00, -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,   0.000,   9.300, Opensky_beacon ,
light.3 = 4,  57.000,   0.000,   3.500, Opensky_Boeing_vclight ,
light.4 = 3,  30.000,   0.000,  -3.000, Opensky_nacelle_refl ,   // front cargo
light.5 = 3, -33.000,   0.000,  -2.000, Opensky_nacelle_refl ,   // rear cargo
light.6 = 3,  40.000,   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= 8,  30.000,  -6.200,  -1.000, Opensky_nacelle_refl ,   // wing/LE slat rays from inspection lights
light.12= 8,  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,  60.000,   0.000, -12.550, Opensky-taxi-refl    ,   // gear bay taxi light rays from taxi lights
light.16= 3, -62.000,   0.000,   7.000, Opensky_nav_yellow   ,   // Tail Nav Light
light.17= 2, -62.000,   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 = 3
exit_rate.0 = 0.10 ;Percent per second
exit_rate.1 = 0.12 ;Percent per second
exit_rate.2 = 0.12 ;Percent per second


[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.12,0.11                          ;Percent per second


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


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
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 = 2                    
electric_pump=1


[airplane_geometry]
wing_area               = 1137.000
wing_span               =  117.500
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      =    1
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           =  -60.000
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           =  -53.000
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           =   45.000
spoilerons_available    =    1
aileron_to_spoileron_gain = 1.000
min_ailerons_for_spoilerons=10.000
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    = 165.000
full_flaps_stall_speed  = 132.000
cruise_speed            = 452.160
max_mach                = 0.825
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                                    // 
flaps-position.1 = 20                                   // 
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    = 0.6                                  // 0.0 .. 1.0
extending-time   = 36                                   // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 10                                   // 
flaps-position.2 = 20                                   // 
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
