[fltsim.0]
title=Beagle Basset 1
sim=Beagle Basset
model=
panel=
sound=
texture=1
kb_checklists=Beagle_Basset_check
kb_reference=Beagle_Basset_ref
atc_id=XS777
ui_manufacturer=Beagle Aircraft Ltd
ui_type=Basset
ui_variation= XS777
ui_typerole="Twin Engine Prop"
ui_createdby="robcarrich"
description=The design of a twin-engined light transport began in 1960 and the prototype registered "G-ARRM" (designated the B.206X) first flew from Shoreham Airport, West Sussex on 15 August 1961.The prototype aircraft was a five-seat all metal low-wing monoplane powered by two Continental flat-six engines.The Beagle B.206 was slightly larger with a larger span wing and seating for seven. Two aircraft were built for evaluation by the Ministry of Aviation at Boscombe Down and an order for twenty aircraft for the Royal Air Force followed. The RAF aircraft were named the Beagle Basset CC.1 and were built at Rearsby Aerodrome, Leicestershire.Series 2 aircraft with 340hp Continental turbocharged engines first flew on 23 June 1965. The Series 2 was also fitted with a large freight door. The aircraft was soon in demand with air taxi companies and as a light transport for companies. Two aircraft were delivered to the Royal Flying Doctor Service in Australia.Series 3 was developed with a raised rear fuselage to carry 10-passengers but only three were built. When the company needed the room at Rearsby to built the Beagle Pup, production of the B.206 ended with the 85th aircraft.
The first deliveries to RAF communications squadrons was made in May 1965. It was powered by two Rolls Royce/Continental GIO-470 six cylinder horizontally-opposed engines giving it a maximum speed of 220 mph and a range of 1,645 miles. Up to eight persons could be carried. A competition was held at Northolt in March 1963 between the B206 and the Devon for an aircraft to replace the Avro Anson,resulting in 20 Bassets being ordered for the RAF.The Northolt aircraft were originally based at RAF Bovingdon near Watford in Hertfordshire with the Southern Communications Squadron until the 'SCS' moved to Northolt and became 207sqn on 4th February 1969. Another squadron, the Northern Communications Squadron, operated Bassets from RAF Topcliffe near Thirsk in North Yorkshire, later becoming 26sqn at RAF Wyton. Most aircraft were removed from RAF service on 2nd May 1974 and sold for civil use.The first civil ordered aircraft was also delivered in May 1965 to Rolls-Royce Limited at Hucknall.An unusual use for one of the first aircraft registered "G-ATHO" which was bought by the Maidenhead Organ Studios Limited for transporting electronic organs.
[fltsim.1]
title=Beagle Basset 2
sim=Beagle Basset
model=
panel=
sound=
texture=2
kb_checklists=Beagle_Basset_check
kb_reference=Beagle_Basset_ref
atc_id=XS770
ui_manufacturer=Beagle Aircraft Ltd
ui_type=Basset
ui_variation=XS770
ui_typerole="Twin Engine Prop"
ui_createdby="robcarrich"
description=The design of a twin-engined light transport began in 1960 and the prototype registered "G-ARRM" (designated the B.206X) first flew from Shoreham Airport, West Sussex on 15 August 1961.The prototype aircraft was a five-seat all metal low-wing monoplane powered by two Continental flat-six engines.The Beagle B.206 was slightly larger with a larger span wing and seating for seven. Two aircraft were built for evaluation by the Ministry of Aviation at Boscombe Down and an order for twenty aircraft for the Royal Air Force followed. The RAF aircraft were named the Beagle Basset CC.1 and were built at Rearsby Aerodrome, Leicestershire.Series 2 aircraft with 340hp Continental turbocharged engines first flew on 23 June 1965. The Series 2 was also fitted with a large freight door. The aircraft was soon in demand with air taxi companies and as a light transport for companies. Two aircraft were delivered to the Royal Flying Doctor Service in Australia.Series 3 was developed with a raised rear fuselage to carry 10-passengers but only three were built. When the company needed the room at Rearsby to built the Beagle Pup, production of the B.206 ended with the 85th aircraft.
The first deliveries to RAF communications squadrons was made in May 1965. It was powered by two Rolls Royce/Continental GIO-470 six cylinder horizontally-opposed engines giving it a maximum speed of 220 mph and a range of 1,645 miles. Up to eight persons could be carried. A competition was held at Northolt in March 1963 between the B206 and the Devon for an aircraft to replace the Avro Anson, resulting in 20 Bassets being ordered for the RAF.The Northolt aircraft were originally based at RAF Bovingdon near Watford in Hertfordshire with the Southern Communications Squadron until the 'SCS' moved to Northolt and became 207sqn on 4th February 1969. Another squadron, the Northern Communications Squadron, operated Bassets from RAF Topcliffe near Thirsk in North Yorkshire, later becoming 26sqn at RAF Wyton. Most aircraft were removed from RAF service on 2nd May 1974 and sold for civil use.The first civil ordered aircraft was also delivered in May 1965 to Rolls-Royce Limited at Hucknall.An unusual use for one of the first aircraft registered "G-ATHO" which was bought by the Maidenhead Organ Studios Limited for transporting electronic organs.
[General]
atc_type=basset
atc_model=CC1
editable=1
performance="Cruise Speed\175 kts\/hr,Engine, Teledyne Continental Motors IO-550-C 300 hp,Propeller\Two-bladed McCauley constant-speed, variable pitch,Maximum Range, 1,569 nm 2,906 km,Service Ceiling, 20,688 ft 6,306 km,Fuel Capacity, 142 gal 537 L,Maximum Gross Weight, 7.125 lb,Length, 29 ft, 10 in 9.09 m,Wingspan, 37 ft, 10 in 11.53 m,Height, 9 ft, 9 in 2.97 m
Seating Up to 8.Useful Load, 1,613 lb"
Category =airplane
[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 11.5, 0.7, -0.2
InitialPbh = 5, 0, 275
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -11.5, 0.6, -0.2
InitialPbh = 5, 0, 85
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 2.0, -15.0
InitialPbh = 7, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.3]
Title = "Nose"
Guid = {3D31E848-6F6F-45d4-8E43-6290708756E3}
Description = Looking back from the nose toward the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.6
ShowWeather = Yes
InitialXyz = -2.0, 0.80, 7.50
InitialPbh = 5.0, 0.0, 165
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum
[CameraDefinition.4]
Title = "Nose Gear"
Guid = {5517F522-6C47-40da-BE66-3D7E10520D75}
Description = Looking back from the nose gear
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .6
ShowWeather = Yes
InitialXyz = 0, -0.9, 7.90
InitialPbh = 0, 0.0, 180
XyzAdjust = TRUE
Category = Aircraft
MomentumEffect = FALSE
ClipMode = Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 0.70
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.7, 0.1, -0.1
InitialPbh=3, 0, 0
[CameraDefinition.002]
Title = "Radio Stack"
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 = 0.6
SmoothZoomTime = 2.0
ZoomPanScalar = 0.70
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.41, -0.09, -0.1
InitialPbh=15, 0, 0
[CameraDefinition.003]
Title = "Engine Controls"
Guid = {563fdda0-af36-4c28-ab71-b5db7e77e474}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 0.60
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.27, -0.1, 0.0
InitialPbh=45, 0, 0
[CameraDefinition.004]
Title = "passenger window"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = yes
SnapPbhAdjust = None
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 0.80
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=-40
InitialXyz=-0.0, -0.060, -1.71
InitialPbh=10.0, 0.0, 70.0
[CameraDefinition.005]
Title = "passenger"
Guid = {18EF1F08-7138-4530-948C-07698E51940D}
Origin = Virtual Cockpit
MomentumEffect = yes
SnapPbhAdjust = None
SnapPbhReturn = True
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = TRUE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 0.80
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare = FALSE
Category = Cockpit
PitchPanRate = 30
HeadingPanRate =60
InitialXyz = 0.80, -0.060, -1.7130
InitialPbh = 10.0, 0.0,-70.0
[WEIGHT_AND_BALANCE]
max_gross_weight =7125.00000 // (pounds)
empty_weight =4365.00000 // (pounds)
reference_datum_position = 0.0000, 0.0000, 0.0000 // (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 =6
station_load.0 = 170, 0.00, -1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, 0.00, 1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 170, -1.80, -1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 170, -1.80, 1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.4 = 0, -12.67, 1.1, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.5 = 0, -15.00, 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 = "Passenger"
station_name.3 = "Passenger"
//station_name.4 = "Passenger"
//station_name.5 = "Passenger"
//station_name.6 = "Baggage"
;Moments of Inertia
empty_weight_pitch_MOI =4415.36000
empty_weight_roll_MOI =2988.34000
empty_weight_yaw_MOI =5878.49000
empty_weight_coupled_MOI=0.00000
[flight_tuning]
cruise_lift_scalar =1.00000
parasite_drag_scalar =0.80000
induced_drag_scalar =0.80000
elevator_effectiveness =1.00000
aileron_effectiveness =1.00000
rudder_effectiveness =1.80000
pitch_stability =1.00000
roll_stability =1.00000
yaw_stability =1.00000
elevator_trim_effectiveness =1.50000
aileron_trim_effectiveness =1.00000
rudder_trim_effectiveness =1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000
[GeneralEngineData]
engine_type =0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 =1.400, -7.00, -0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 =1.400, 7.00, -0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.00000 //Fuel flow scalar
min_throttle_limit =0.00000; //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar =1.00000 //Piston power scalar
cylinder_displacement=91.70000 //Cubic inches per cylinder
compression_ratio=8.00000 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm=2700.00000 //Max rated RPM
max_rated_hp=300.00000 //Max rated HP
fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.30415 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=49.92000 //Max design manifold pressure, (inHg)
min_design_mp=2.99200 //Min design manifold pressure, (inHg)
critical_altitude=0.00000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0.00000 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0.00000 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.00000 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.00000 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.00000 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.00000 //Scalar on idle RPM friction
emergency_boost_duration=0.00000
BestPowerSpecificFuelConsumption=0.50000
[propeller]
thrust_scalar =1.00000 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.40000 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=6.64510 //Propeller moment of inertia
beta_max=45.00000 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.20000 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1100.00000 //Miminum governed RPM
prop_tc=0.10000 //Prop time-constant
gear_reduction_ratio=1.00000 //Propeller gear reduction ratio
fixed_pitch_beta=0.00000 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.00000 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700.00000 //Minimum RPM for prop feathering
beta_feather=82.50000 //Feathering pitch angle (degrees)
power_absorbed_cf=0.90000 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0.00000 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.00000 //Minimum pitch angle in reverse, (degrees)
[contact_points]
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 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)
//GEAR
//SCRAPES
static_pitch = 0.661 //degrees (pitch when loaded on ground)
static_cg_height= 4.835 //feet, altitude of CG when at rest on the ground
gear_system_type=0 //Electric
max_number_of_points=7
point.0= 1, 8.098, 0.000, -4.850, 2600, 0, 0.633, 45.000, 0.320, 2.000, 0.600, 3.000, 3.000, 0, 152.1, 179.9
point.1= 1, -1.512, -7.180, -4.80, 2600, 1, 0.886, 0.000, 0.400, 0.100, 0.100, 4.100, 4.300, 2, 152.1, 199.9
point.2= 1, -1.512, 7.180, -4.80, 2600, 2, 0.886, 0.000, 0.400, 0.100, 0.100, 4.100, 4.100, 3, 152.1, 199.9
point.3= 2, -6.200, -18.910, 0.500, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -6.200, 18.910, 0.500, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -24.040, 0.000, -0.500, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 0.400, 0.000, -1.240, 800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
tailwheel_lock=0
[gear_warning_system]
gear_warning_available =1 //Normal
pct_throttle_limit =0.10000 //Percent throttle that activates warning
flap_limit_idle =22.50000 //Flap angle that activates warning at idle
flap_limit_power =31.50000 //Flap angle that activates warning at above idle
[brakes]
parking_brake =1 //Parking brake available
toe_brakes_scale =1.00000 //Brake scalar
auto_brakes =0
hydraulic_system_scalar=1.00000
differential_braking_scale=1.00000
[hydraulic_system]
normal_pressure =500.00000 //PSI
engine_map=1,1,0,0
[flaps.0]
type= 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
system_type=4 //Electric
span-outboard= 0.410 // 0.0 .. 1.0
extending-time= 4.0 // seconds
damaging-speed=152.0 // KIAS
blowout-speed=250.0 // KIAS
flaps-position.0=0.00 // degrees
flaps-position.1=15.00 // degrees
flaps-position.2=25.00 // degrees
flaps-position.3=35.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=0.00
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[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, 0
Adf.1 = 1
Transponder.1 = 1
Marker.1 = 1
[Views]
eyepoint = 1.5, -1.20, 2.5 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0 =4, 1.5, 0.00, 2.5, fx_vclight
light.1 =3, -6.820000, 19.290000, 1.170000,
light.2 =3, -21.793000, 0.000000, 0.802000, fx_navwhi
light.3 =2, -6.480000, -19.040000, 1.170000,
light.4 =2, -6.480000, 19.040000, 1.170000,
light.5 =1, -1.115000, 0.000000, 3.642000, fx_beacon
light.6 =2, -1.115000, 0.010000, 3.642000, fx_strobe
light.7 =1, -9.940000, 0.000000, -1.779000, fx_beacon
[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 //Square feet
aileron = 150, 250 //Square feet
rudder = 150, 250 //Square feet
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=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
direction_indicator.1=3,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1
attitude_indicator.1=1
//[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
//turn_indicator.0=1,2 //Turn and Bank
//turn_indicator.1=1,2
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=4.900000
engine_map=1,1
[pneumatic_system]
max_pressure=250.000000 //PSI
bleed_air_scalar=1.00000
[fuel]
LeftMain = -0.000, -6.450, 0.000, 97.500, 0.000 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -0.000, 6.450, 0.000, 97.500, 0.000 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type =1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =2
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0
[EFFECTS]
wake=fx_wake
water=fx_spray // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 3
exit.0 = 0.4 // (0=Main 1=Emergency)
exit.1 = 0.4 // (0=Main 1=Emergency)
[airplane_geometry]
wing_area =214.00000 //Square feet
wing_span =46.0000 //Feet
wing_root_chord =7.00000 //Feet
wing_dihedral =4.90000 //Degrees
wing_incidence =0.00000 //Degrees
wing_twist =0.00000 //Degrees
oswald_efficiency_factor=0.70000 //Measure of lift effeciency of wing
wing_winglets_flag =0 //Are winglets available?
wing_sweep =0.00000 //Degrees, wing leading edge
wing_pos_apex_lon =0.00000 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert =-1.30000 //Feet, vertical distance from reference point, positive going up
htail_area =60.00000 //Square feet
htail_span =17.90000 //Feet
htail_pos_lon =-18.5000 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert =0.70000 //Feet, vertical distance from reference point, positive going up
htail_incidence =0.00000 //Degrees
htail_sweep =0.00000 //Degrees, horizontal tail leading edge
vtail_area =18.00000 //Square feet
vtail_span =10.70000 //Feet, tip to body
vtail_sweep =55.00000 //Degrees, vertical tail leading edge
vtail_pos_lon =-19.16000 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert =3.10000 //Feet, vertical distance from reference point, positive going up
elevator_area =20.00000 //Square feet
aileron_area =11.30000 //Square feet
rudder_area =10.50000 //Square feet
elevator_up_limit =17.00000 //Degrees
elevator_down_limit =15.50000 //Degrees
aileron_up_limit =18.00000 //Degrees
aileron_down_limit =18.00000 //Degrees
rudder_limit =30.00000 //Degrees
elevator_trim_limit =15.00000 //Degrees
spoiler_limit =0.00000 //Degrees
spoilerons_available =0 //Spoilerons Available?
aileron_to_spoileron_gain =0.00000 //Aileron to spoileron gain
min_ailerons_for_spoilerons =0.00000 //Degrees
min_flaps_for_spoilerons =0.00000 //Minimum flap handle position when spoilerons activate
auto_spoiler_available =0
positive_g_limit_flaps_up =3.00000 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=2.10000 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up =-2.40000 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-1.80000 //Design G load tolerance (negative, flaps down)
load_safety_factor =1.50000 //Design G load safety factor
spoiler_extension_time=0.00000
spoiler_handle_available=0
[Reference Speeds]
flaps_up_stall_speed = 84.0 //Knots True (KTAS)
full_flaps_stall_speed = 75.0 //Knots True (KTAS)
cruise_speed =179.96505 //Knots True (KTAS)
max_indicated_speed =222.97939 //Red line (KIAS)
max_mach=0.31000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700
autothrottle_available=0
pitch_takeoff_ga=8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =0
default_pitch_mode=0
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
use_no_default_bank=1
use_no_default_pitch=1
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=1000 ; 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 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
stick_shaker=0 ; 0 - 10000
[deice_system]
structural_deice_type=3 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[AirWrench]
Aircraft_Length=30.24000
nose_position_lon=8.88000
Vmax_sl=236.10000
Vmax_ca=236.10000
V_si=74.20000
V_so=66.60000
V_rc=93.60000
Climb_Rate=2132.30000
Climb_Weight=4933.00000
Max_gforce=4.50000
Emergency_hp=300.00000
VSI_Weight=4081.00000
static_margin=0.13300
ActualIncidence=1.00000
ActualTwist=-1.00000
ActualTailIncidence=0.50000
Aircraft_Type=2
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=675.00000
piston_research=0.00000
Max_Prop_Eff=0.87000
JetAltitude=0.00000
turboprop_critical_altitude=0.00000
target_roll_Vopt=342.50000
target_roll_rate=45.80000
zero_roll_mph=765.80000
pitch_damping=1.00000
yaw_damping=1.00000
roll_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.00000
rudder_scalar=1.50000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=0.00000
Aileron_FF=0.00000
Roll_Response=30.00000
Adverse_Yaw=100.00000
Control_Response=100.00000
V_Max_Control=256.62372
V_Zero_Control=513.24743
V_Max_RdrControl=256.60000
V_Zero_RdrControl=513.20000
Spin_Stability=100.00000
Roll_Off=0.00000
glide_ratio=11.90931
vn_gmax=4.50000
vn_vmo=256.62372
expert_mode=0
CritAoA=16.00000
ClAoA_k0=1.00000
ClAoA_k1=1.00000
ClAoA_k2=0.85000
ClAoA_k3=0.80000
cruise_attitude=0.00000
Elevator_Propwash=1.00000
Rudder_Propwash=1.50000
afterburner_thrust=0.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=0
spoiler_cd=0.04790
spoiler_cl=-0.09000
spoiler_cm=0.00000
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.39000
flaps_cm_scalar=-0.52400
vfe_enabled=0
gear_cd_scalar=0.35000
gear_cm_scalar=-0.00000
critical_mach_number=0.80000
max_mach_cd0=60
cylinder_head_temperature=501.00000
exhaust_gas_temperature=1201.00000
fuel_pressure=40.00000
oil_pressure=60.00000
oil_temperature=241.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=0.00000
interstage_turbine_temperature=-459.00000
RAM_Jet_Effect=1.00000
Emulate_Turbojet=0
N2_idle=66.00000
jet_idle_scalar=1.00000
input_units=0
fs_version=7
AI_flag=0
edit_tp_torque=0
keep_jet_air_defs=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=10000
range_est_rpm=2700.00000
range_est_mp=29.92000
range_est_fuel=142.00000
contact_light_flags=0
AirWrenchVersion=1.01.86
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
[turn_indicators]
turn_indicator.0=1,0
