[fltsim.0]
title=hoverV2
sim=hama_hover
model=hover_v2
panel=
sound=
texture=hover
kb_checklists=
kb_reference=
atc_id_color=
atc_id=
atc_airline=
atc_flight_number=1123
atc_parking_types=
ui_manufacturer=Ship
ui_type=Hovercraft V03
ui_variation=FS2004
//--- FSX cameras
[CameraDefinition.0]
Title = "External view frontside"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = External view bow
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
ShowWeather = Yes
InitialXyz= 6.3,3.0, 18.0
InitialPbh=17.0,0.0,206.0 //qu,lä,ho
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Behind the stern"
Guid = {B9EC0805-43B8-430f-9BEB-5C68A45C33EC}
Description = Looking forwards
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.4
ShowWeather = Yes
InitialXyz = 5.8,3.6,-23
InitialPbh = 9.0,0.0,-22
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.2]
Title = "External view to the stern portside"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = "Looking forwards"
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
ShowWeather = Yes
InitialXyz =-20,3,-30
InitialPbh = 5,0, 38
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
[CameraDefinition.3]
Title = "At the door_Shift E"
Guid={DF40A5DF-A129-4117-8075-9F4FA6DBFE2C}
Description = "Open the doors"
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.3
ShowWeather=Yes
InitialXyz=-7.9,2.0,-5.0
InitialPbh= 0.0,0.0,98.0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.4]
Title = "External view to portside"
Guid = {B0CA7E72-F3D9-F748-8BF5-108D197B2469}
Description = "abc"
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
ShowWeather = Yes
InitialXyz =-20, 5.6, 0
InitialPbh = 15, 0.0,90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
---
[CameraDefinition.001]
Title = "Center console"
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 = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.2,0.0, 0.2
InitialPbh=50.0,0.0,-45.0 //qu,lä,ho
[CameraDefinition.002]
Title = "Passenger seat front left"
Guid = {195EAB58-9E4A-2E2A-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 = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-2.2,0.3,-2.7
InitialPbh= 4.0,0.0,45.0 //qu,lä,ho
[CameraDefinition.003]
Title = "Passenger seat front right"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
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 = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= 1.3,0.0,-2.5
InitialPbh= 0.0,0.0,45.0
[CameraDefinition.004]
Title = "Stewardess at aisle"
Guid = {195EAB58-9E4A-4E2A-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 = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= 0.7,0.1,-1.4
InitialPbh= 8.0,0.0,180.0 //qu,lä,ho
[CameraDefinition.005]
Title = "Passenger view forward left"
Guid = {195EAB58-9E4A-5E2A-A34C-A8D9D948F078}
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=20
HeadingPanRate=60
InitialXyz= 2.1,0.2, -8.0
InitialPbh= 0.0,0.0,-45.0 //qu,lä,ho
[CameraDefinition.006]
Title = "Passenger view to the left door_Shift E"
Guid = {195EAB58-9E4A-6E2A-A34C-A8D9D948F078}
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=20
HeadingPanRate=60
InitialXyz= 0.5,0.0, -8.0
InitialPbh= 0.0,0.0,-125.0 //qu,lä,ho
//-----------------------------------------------
[General]
atc_type=
atc_model=
editable=0
performance="Maximum Speed\n 90 km\/hr\n\nLength\n 23.1 m\n\nspan 11 m\n\nHeight 4.8 m\n\nSeating 105"
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight=8000 // (pounds)
empty_weight=4895 // (pounds)
reference_datum_position=13.1, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-13.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0 = "170.0, -11.3, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, -11.3, 1.5, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "160.0, -13.9, -2.0, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "160.0, -13.9, 2.0, 0.0, Passenger 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0.0, -18.8, -2.0, 0.0, Passenger 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "0.0, -18.8, 2.0, 0.0, Passenger 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = " 50.0, -21.0, 0.0, 0.0, Cargo Zone 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "25.0, -23.5, 0.0, 0.0, Cargo Zone 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0.0, -25.6, 0.0, 0.0, Cargo Zone 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0.0, -27.5, 0.0, 0.0, Cargo Zone 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "0.0, -9.9, -5.3, -6.5, Left Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "0.0, -9.9, 5.3, -6.5, Right Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI=7241.36
empty_weight_roll_MOI=5618.57
empty_weight_yaw_MOI=10431.43
empty_weight_coupled_MOI=0.0
[Flaps.0]
type=1
span-outboard=0.5 // Percent span for flap position
extending-time=5.7 // Seconds, time to fully extend
system_type=0 // 0 = electrical
damaging-speed=175 // KIAS
blowout-speed=175 // KIAS
flaps-position.0=0 // degrees
flaps-position.1=10,175 // degrees
flaps-position.2=20,150 // degrees
flaps-position.3=30,125 // degrees
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-18.3, -2.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-18.3, 2.8, 0.5 //(feet) longitudinal, lateral, vertical distance fromreference datum
fuel_flow_scalar=1.12 //Scalar for fuel flow efficiency
min_throttle_limit=-0.25 //Minimum percent throttle. Generally negative for turbine reverser
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=8.8 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=19 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15.6 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.004 //Prop time-constant
gear_reduction_ratio=17.4 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //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=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=88.0 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain=0.011 //Gain on fuel flow
inlet_area=1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm=33000 //RPM, second stage compressor rated value
static_thrust=158 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar=1.0 //Scalar on Turboprop power
maximum_torque=1865 //Maximum torque available (ft-lbs)
[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
;/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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal
;/11 Extension Time (seconds)
;/12 Retraction Time (seconds)
;/13 Sound Type
;/14 Airspeed limit for retraction (KIAS)
;/15 Airspeed that gear gets damage at (KIAS)
point.0=1, -1.15, -5.250, -5.500, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.80, 4.0, 4.0, 0, 175.0, 175.0
point.1=1, -1.15, 5.250, -5.500, 1600, 0, 1.40, 30.0, 0.3, 2.5, 0.80, 4.0, 4.0, 1, 175.0, 175.0
point.2=1, -16.40, -5.250, -5.500, 1600, 1, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 2, 175.0, 175.0
point.3=1, -16.40, 5.250, -5.500, 1600, 2, 1.50, 0.0, 0.4, 2.5, 0.80, 4.0, 4.0, 3, 175.0, 175.0
point.4=4, -4.00, -5.250, -4.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
point.5=4, -4.00, 5.250, -4.600, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.6=4, -26.35, -5.250, -4.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.7=4, -26.35, 5.250, -4.800, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
point.8=2, -12.90, -26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.9=2, -12.90 26.00, 3.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.10=2, -36.23, 0.00, 0.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.11=2, -0.50, 0.00, -2.17, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.12=2, -38.00, 0.00, 9.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0
point.13=5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
point.14=5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0
max_number_of_points=21
static_pitch=0.983 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.344 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available=2 //Amphib
pct_throttle_limit=0.1 //Percent throttle that activates warning
flap_limit_idle=20.1 //Flap angle that activates warning at idle
flap_limit_power=13.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake=1 //Parking brake available
toe_brakes_scale=0.68 //Brake scalar
[hydraulic_system]
normal_pressure=3000.0 //PSI
electric_pumps=0 //no electric pumps
engine_map=1,0,0,0 //pump on Eng1
[Views]
eyepoint=7.78, 1.9, 7.5 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
light.0=3, -2.90, -7.98, 10.25, fx_navred ,
light.1=3, -2.90, 7.98, 10.25, fx_navgre ,
light.2=2, 2.84, 0.00, 13.65, fx_beacon ,
light.3=4, 8, 0.00, 6, fx_vclighth,
[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, 180
aileron=200, 1000
rudder=200, 1000
[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=1,0
[airspeed_indicators]
airspeed_indicator.0=1.16, -22.0
[EFFECTS]
wake=hama_SRN_1
water=hama_SRN_side
dirt=hama_hover_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
//wake=hama_hover_1
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4 ;Percent per second
[fuel]
LeftMain=-15.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-15.3, 1.1, 2.5, 166.0, 3.6 //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=279.0 //Square feet
wing_span=52.1 //Feet
wing_root_chord=6.4 //Feet
wing_dihedral=3.9 //Degrees
wing_incidence=2.5 //Degrees
wing_twist=-1.7 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.96 //Degrees, wing leading edge
wing_pos_apex_lon=-12.3 //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=39.0 //Square feet
htail_span=11.7 //Feet
htail_pos_lon=-27.8 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0 //Degrees
htail_sweep=5.0 //Degrees, horizontal tail leading edge
vtail_area=18.0 //Square feet
vtail_span=4.8 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-25.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up
elevator_area=16.6 //Square feet
aileron_area=18.3 //Square feet
rudder_area=80.7 //Square feet
elevator_up_limit=28.0 //Degrees
elevator_down_limit=21.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=25.0 //Degrees
rudder_limit=60.0 //Degrees
elevator_trim_limit=19.5 //Degrees
spoiler_limit=20.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=1 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
spoiler_handle_available=0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
auto_spoiler_available=0
spoiler_extension_time=0.200000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[Reference Speeds]
flaps_up_stall_speed=72.0 //Knots True (KCAS)
full_flaps_stall_speed=58.0 //Knots True (KCAS)
cruise_speed=143.0 //Knots True (KTAS)
max_mach=0.60
max_indicated_speed=175 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=1
pitch_takeoff_ga=8.0
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
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=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
[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=0
[pitot_static]
pitot_heat=1.000000
[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=0.150000
[deice_system]
structural_deice_type=0
