Re: I cant Install the 737 in the FSX SE
Posted: Wed Sep 14, 2016 11:32 pm
by OAFP
This is the only way that I find
//FD version 13.11.20.1
//by Tom Falley//
[fltsim.0]
title=Milviz B737-200 CanNorth
sim=737-200
model=cargo
panel=s177
sound=
texture=CANORTH
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=C-GSPW
atc_airline=Boeing
atc_flight_number=
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="CANNORTH"
ui_typerole="Cargo"
ui_createdby="Milviz"
gravel_kit=true
[fltsim.1]
title=Milviz B737-200 Piedmont
sim=737-200
model=pax
panel=s177
sound=
texture=PIEDMONT
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=N775N
atc_airline=Boeing
atc_flight_number=327
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="PIEDMONT_PAX"
ui_typerole="Commercial Airliner"
ui_createdby="Milviz"
gravel_kit=false
[fltsim.2]
title=Milviz B737-200 Firstair
sim=737-200
model=combi
panel=s177
sound=
texture=FIRSTAIR
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=C-GNWN
atc_airline=Boeing
atc_flight_number=327
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="Firstair"
ui_typerole="Combi-Cargo-Pax"
ui_createdby="Milviz"
gravel_kit=true
[fltsim.3]
title=Milviz B737-200 BRAA
sim=737-200
model=pax
panel=s177
sound=
texture=BRAATHENS
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=LN-SUA
atc_airline=Boeing
atc_flight_number=327
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="BRAATHENS_Combi"
ui_typerole="Combi-Cargo-Pax"
ui_createdby="Milviz"
gravel_kit=false
[fltsim.4]
title=Milviz B737-200 Alaska
sim=737-200
model=cargo
panel=s77
sound=
texture=alaska
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=N711AS
atc_airline=Boeing
atc_flight_number=
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="Alaska Airlines"
ui_typerole="Cargo"
ui_createdby="Milviz"
gravel_kit=true
[fltsim.5]
title=Milviz B737-200 Janet
sim=737-200
model=combi
panel=s177
sound=
texture=JANET51
kb_checklists=Milviz_B732_check
kb_reference=Milviz_B732_ref
atc_id=N5294M
atc_airline=Boeing
atc_flight_number=327
ui_manufacturer="Boeing"
ui_type="737-200"
ui_variation="JANET_Pax"
ui_typerole="Combi-Cargo-Pax"
ui_createdby="Milviz"
gravel_kit=false
[General]
atc_type=BOEING
atc_model=B732
editable=0
performance="Cruise Speed \nMach 0.740 437 kts 853 km\/h\n\nEngines \nJT8D-17A\n\nMaximum Range \n3,060 nm 3,521 mi 5,425 km\n\nService Ceiling \n37, 000 ft 9,500 m\n\nFuel Capacity \n6,875 U.S. gal 26,020 L\n\nEmpty Weight-Standard \n67,710 lb \n\nMaximum Gross Weight\n128,200 lb \n\nLength \n96.9 ft 29.53\n\nWingspan \n93.0 feet 28.35 m\n\nHeight \n37.0ft 11.28m\n\nSeating \nSeats 119\n\n"
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 = 0.8
ShowWeather = Yes
InitialXyz = 3.2, 1.8, -5
InitialPbh = 5, 0, 100
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 = 0.8
ShowWeather = Yes
InitialXyz = -3.2, 1.8, -5
InitialPbh = 5, 0, 260
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[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 = .52
ShowWeather = Yes
InitialXyz = -3.3, -1.8, -11
InitialPbh = 0, 0, 17
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[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 = .75
ShowWeather = Yes
InitialXyz = 0, 6.5, -55.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.4]
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.5]
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.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 = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=50
HeadingPanRate=50
InitialXyz=0.94, 0.0, 0.0
InitialPbh=2, 0, 0
[CameraDefinition.002]
Title=Center Console
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.08
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=50
HeadingPanRate=50
InitialXyz=0.45, 0.30, -0.19
InitialPbh=84.2, 0, 0
[CameraDefinition.003]
Title=Engine Controls
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=50
HeadingPanRate=50
InitialXyz=0.45, 0.10, 0.25
InitialPbh=85.0, 0, 0
[CameraDefinition.004]
Title=FMS
Guid = {a5741a54-ea6d-4580-9709-c99161e38a86}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=50
HeadingPanRate=50
InitialXyz=0.45, 0.00, -0.25
InitialPbh=37.0, 0, 0
[CameraDefinition.005]
Title=Overhead Panel
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.70
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=50
HeadingPanRate=50
InitialXyz=0.47, -0.62, -0.4
InitialPbh=-66.7, 0, 0
[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 = 128100 // (pounds)for 2X6C cargo Combi
empty_weight = 67710 // (pounds)
reference_datum_position = 40, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -39.5, -0.00, -2.0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 170, -5.62, 1.5, 3.0 //Captain, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -5.62, -1.5, 3.0 //FO, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 230, -16.28, 0.0, 3.0 //FWD FA Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 2040, -19.98, 0.0, 3.0 //First Class seats. Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 3060, -26.48, 0.0, 3.0 //Fwd Coach A seats, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 3060, -34.19, 0.0, 3.0 //Fwd Coach B seats Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 4080, -44.64, 0.0, 3.0 //Aft Mid Coach seats, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 4080, -54.54, 0.0, 3.0 //Aft Coach A seats, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 3910, -64.39, 0.0, 3.0 //Aft Coach B seats, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 230, -68.28, 0.0, 3.0 //AFT FA Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = 2000, -23.66, 0.0, -3.0 //Fwd cargo, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = 1860, -60.15, 0.0, -3.0 //Aft Cargo, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.12 = 0, -19.00, 0.0, -3.0 //Pallete 1, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.13 = 0, -26.28, 0.0, -3.0 //Pallete 2, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.14 = 0, -33.63, 0.0, -3.0 //Pallete 3, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.15 = 0, -40.86, 0.0, -3.0 //Pallete 4, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.16 = 0, -48.47, 0.0, -3.0 //Pallete 5, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.17 = 0, -55.77, 0.0, -3.0 //Pallete 6, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.18 = 0, -63.11, 0.0, -3.0 //Pallete 7, Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Fwd Crew"
station_name.3 = "First Class"
station_name.4 = "Fwd Coach A"
station_name.5 = "Fwd Coach B"
station_name.6 = "Aft Mid Coach"
station_name.7 = "Aft Coach A"
station_name.8 = "Aft Coach B"
station_name.9 = "Aft Crew"
station_name.10 = "Forward Baggage"
station_name.11 = "Aft Baggage"
station_name.12 = "Pallete 1"
station_name.13 = "Pallete 2"
station_name.14 = "Pallete 3"
station_name.15 = "Pallete 4"
station_name.16 = "Pallete 5"
station_name.17 = "Pallete 6"
station_name.18 = "Pallete 7"
;Moments of Inertia
empty_weight_pitch_MOI = 330655
empty_weight_roll_MOI = 488050
empty_weight_yaw_MOI = 468751
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar = 1.15 //1.05
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
[SMOKESYSTEM]
//smoke.1= -70.0, -15.5, -1.0, Milviz_B737_Smoke
//smoke.2= -70.0, 15.5, -1.0, Milviz_B737_Smoke
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.1 = -42.0, -14.0, -1.0
Engine.2 = -42.0, 14.018, -1.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.19 //Scalar for fuel flow efficiency
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
[TurbineEngineData]
fuel_flow_gain = 0.0030 //Gain on fuel flow
inlet_area = 11.4 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 14500 //Lbs, max rated static thrust at Sea Level JTD17A
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.653 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 0 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 1.0
[electrical]
// ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 1, 5 , 17.0
flap_motor = 0, 0 , 1.0
avionics_bus = 0, 0 , 17.0
avionics = 1, 25 , 17.0
pitot_heat = 0, 15 , 17.0
additional_system = 0, 30 , 17.0
marker_beacon = 1, 1 , 17.0
gear_warning = 7, 0 , 17.0
gear_motor = 4, 1 , 17.0
fuel_pump = 0, 5 , 17.0
fuel_transfer_pump = 0, 5 , 17.0
apu_starter = 2, 50, 17.0
starter1 = 2, 20, 17.0
starter2 = 0, 0 , 17.0
light_nav = 0, 10 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 20 , 17.0
light_taxi = 0, 10 , 17.0
light_strobe = 0, 10 , 17.0
light_panel = 0, 7 , 17.0
light_recognition = 0, 5 , 17.0
light_wing = 0, 5 , 17.0
light_cabin= 0, 20, 17.0
standby_vacuum = 0, 0 , 17.0
auto_brakes = 0, 0 , 17.0
hydraulic_pump = 0, 10 , 17.0
max_battery_voltage = 24
generator_alternator_voltage= 29.5
max_generator_alternator_amps= 400
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
//0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0=1, -13.76, 0.00, -6.60, 2600, 0, 1.442, 55.92, 0.36, 1.8, 0.50, 6.0, 4.0, 1, 270.0, 195.0
point.1=1, -49.05, -8.72, -6.97, 1600, 1, 1.342, 0.00, 0.71, 1.6, 0.50, 6.0, 4.0, 2, 270.0, 225.0
point.2=1, -49.05, 8.72, -6.97, 1600, 2, 1.342, 0.00, 0.71, 1.6, 0.50, 6.0, 4.0, 2, 270.0, 225.0
//point.3=2, -29.00, -48.00, 04.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
//point.4=2, -29.00, 48.00, 04.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
//point.5=2, -43.00, 0.00, 6.80, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
//point.6=2, -61.00, 0.00, 31.00, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
//point.7=2, 44.00, 0.00, 6.50, 1000, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch=-0.3 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 6.45 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.0 //Percent throttle that activates warning
flap_limit_idle = 20.5 //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 = 1.250 //Brake scalar
auto_brakes = 0
hydraulic_system_scalar = 1.0 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
differential_braking_scale = 1.0
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 2 //electric pump
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -3.86, -1.55, 6.32 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 30 // 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 = 1.00
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.25 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0.5
flaps-position.4 = 1.0 //
damaging-speed = 270 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.1
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
flaps-position.4 = 2.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 1
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 10=cabin
light.0=1, -14.00, 0.00, 5.00, fx_vclighth.fx
light.1=1, -28.00, 0.00, 5.00, fx_vclighth.fx
light.2=1, -38.00, 0.00, 5.00, fx_vclighth.fx
light.3=1, -56.00, 0.00, 5.00, fx_vclighth.fx
light.4=1, -72.00, 0.00, 5.00, fx_vclighth.fx
[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 = 250, 350
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
direction_indicator.1=3,0
[altimeters]
altimeter.0=1
altimeter.1=1
[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
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[vacuum_system]
max_pressure=5.15 // PSI
vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
[pneumatic_system]
max_pressure=32.000000
bleed_air_scalar=1.0
[exits]
number_of_exits = 4
exit.0 = 0.4, -12.5, -5.1, 4.9, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -38.5, 4.5, -3.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, 33.5, 3.5, -4.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.3 = 0.4, -24.5, 5.5, -5.2, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 98
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 13.0
max_pitch=13.0
use_no_default_pitch=0 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank=0 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=0.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25,15,10
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.18
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 19.5
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
[fuel]
Center1 = -42.9, 0.0, -0, 2062, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -49.7, -12.2, -0, 1488, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -49.7, 12.2, -0, 1488, 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
[airplane_geometry]
wing_area = 1044.0 //Square feet
wing_span = 93.0 //Feet
wing_root_chord = 19.0 //Feet
wing_dihedral = 5.5 //Degrees
wing_incidence = 1.0 //Degrees
wing_twist = -0.5 //Degrees
oswald_efficiency_factor= 0.78 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 25.0 //Degrees, wing leading edge
wing_pos_apex_lon = -31.04 //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 = 313.6 //Square feet
htail_span = 36.0 //Feet
htail_pos_lon = -100.5 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 8.4 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 30.0 //Degrees, horizontal tail leading edge
vtail_area = 283.0 //Square feet
vtail_span = 23.0 //Feet, tip to body
vtail_sweep = 36.3 //Degrees, vertical tail leading edge
vtail_pos_lon = -96.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 22.9 //Feet, vertical distance from reference point, positive going up
elevator_area = 99.5 //Square feet
aileron_area = 32.9 //Square feet
rudder_area = 66.2 //Square feet
elevator_up_limit = 25.5 //Degrees
elevator_down_limit = 19.5 //Degrees
aileron_up_limit = 25.0 //Degrees
aileron_down_limit = 20.0 //Degrees
rudder_limit = 26.0 //Degrees
elevator_trim_limit = 17.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 2.0 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 2 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 3 //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 = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 113.0 //Knots True (KTAS)
cruise_speed = 437.0 //Knots True (KTAS)
max_mach = 0.840
max_indicated_speed = 362 //Red line (KIAS)
[stall_warning]
type=2
stick_shaker=1
[deice_system]
structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Pressurization]
design_cabin_pressure = 10.90 ;PSI (~8000 feet)
max_pressure_differential = 7.80 ;PSI
[GPWS]
max_warning_height = -1 //No need for GPWS
sink_rate_fpm=-999999
excessive_sink_rate_fpm=-999999
climbout_sink_rate_fpm=-999999
flap_and_gear_sink_rate_fpm=-999999