[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