; Localized 09/12/2006 03:16 AM (GMT) 4:4.2.169 aircraft.cfg [fltsim.0] title=Antonov AN-124 Volga Dnepr sim=an124 model= panel= sound= texture=VD kb_checklists= kb_reference= description=The Anotonov-124 "Ruslan" has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). This paint scheme shows the design of the late eighties. Model and Textures by Tom Ruth. Modified defauld 747400 aircraft.cfg by Alexander Kvitta and Thomas Ruth. Copyright August 2003 ui_manufacturer=Antonov ui_type=AN124 ui_variation=Volga Dnepr ui_typerole=Heavy Freighter ui_createdby=Tom atc_heavy=1 atc_id=82078 atc_airline=VOLGA DNEPR atc_parking_types=CARGO,MIL_CARGO,RAMP atc_flight_number=8278 [fltsim.1] title=Antonov AN-124 White sim=an124 model= panel= sound= texture=WHITE kb_checklists= kb_reference= description=The Anotonov-124 "Ruslan" has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). This paint scheme shows the design of the late eighties. Model and Textures by Tom Ruth. Modified defauld 747400 aircraft.cfg by Alexander Kvitta and Thomas Ruth. Copyright August 2003 ui_manufacturer=Antonov ui_type=AN124 ui_variation=White ui_typerole=Heavy Freighter ui_createdby=Tom atc_heavy=1 atc_id=82078 atc_airline=ANTONOV atc_parking_types=CARGO,MIL_CARGO,RAMP atc_flight_number=8278 [General] atc_type=ANTONOV atc_model=A124 editable=1 performance=4 LotarevD-18T with 229.5kN each MTOW: 402 metrical tons MaxPayload 150 metrical tons Cruise speed:870km/h Max Mach 0.77 Max payload range:4500km Max fuel range: 15400km Max ceiling: 12000 meters Category=airplane [CameraDefinition.0] Title=Right Wingview Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description=Starboard wing as seen from the Flightdeck Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=1.0 ShowWeather=Yes InitialXyz=1.71, 2.79, 18.21 InitialPbh=2, 0, 150 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title=Left Wingview Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description=Port wing as seen from the Flightdeck Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=1.0 ShowWeather=Yes InitialXyz=-1.71, 2.79, 18.21 InitialPbh=2, 0, 220 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.2] Title=Tail Camera Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description=Whole aircraft as seen from the tip of the vertical stabilizer Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.3 ShowWeather=Yes InitialXyz=0, 15.06, -38.32 InitialPbh=10, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.3] Title=Belly Camera Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c} Description=Main gear from the bottom of the aircraft Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.75 ShowWeather=Yes InitialXyz=0, -5.39, -11.67 InitialPbh=0, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.4] Title=Nose Gear Camera Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59} Description=Camera attached to the portside nosegear Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=1.0 ShowWeather=Yes InitialXyz=-0.94, -5.32, 15.89 InitialPbh=0, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum [CameraDefinition.5] Title=Cargodeck Surveillance Front Guid={15501D82-C0F9-40bd-9335-BED496704AB7} Description=Surveillance camera on the cargodeck roof. Pointing to the nose Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=0, -0.29, 13.75 InitialPbh=2, 0, 180 XyzAdjust=TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum [CameraDefinition.6] Title=Cargodeck Surveillance Rear Guid={DF40A5DF-A129-4117-8075-9F4FA6DBFE2C} Description=Surveillance camera on the cargodeck roof. Pointing to the stern Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=0, 0.83, -23-23 InitialPbh=2, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=FALSE 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=.75 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=1.2, 0.0, 0.0 InitialPbh=0, 0, 0 [CameraDefinition.002] Title=Radio Operator 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=0.20, 0, -1.85 InitialPbh=0, 0, 270 [CameraDefinition.003] Title=Navigator Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe} 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=0.20, 0, -1.10 InitialPbh=-0, 0, 270 [CameraDefinition.004] Title=Engineer Guid={4479D678-F256-4302-9BF7-D90C10D17165} 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=1.05, 0, -1.10 InitialPbh=0, 0, 90 [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 = 924198 // (pounds) empty_weight = 395428 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -23, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170.0, 59.7, 2.0, 8.5 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170.0, 59.7, -2.0, 8.5 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=700.0, 50.9, 0.0, 8.5 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=1540.0, 36.7, 0.0, 8.5 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=2140.0, -43.0, 0.0, 8.5 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=10000.0, 30.0, 0.0, -2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=10000.0, 0.0, 0.0, -2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=10000.0, -30.0, 0.0, -2.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0=Pilot station_name.1=Co-Pilot station_name.2=Cockpitcrew station_name.3=Upper Crewdeck station_name.4=Upper Paxdeck station_name.5=Cargo Front station_name.6=Cargo Center station_name.7=Cargo Rear ;Moments of Inertia empty_weight_roll_MOI=13352310 empty_weight_pitch_MOI=24223159 empty_weight_yaw_MOI=39531785 empty_weight_coupled_MOI=0 CG_forward_limit = 0.000 CG_aft_limit = 1.000 [fuel] LeftMain = -23.0, -28.0, 4.0, 27027.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -23.0, 28.0, 4.0, 27027.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -23.0, -36.5, 3.0, 6784.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -23.0, 36.5, 3.0, 6784.0, 0.0 //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 fuel_dump_rate=0.0167 //Percent of max quantity per second, i.e. about 1 minute for full fuel [airplane_geometry] wing_area=7125.0 //Square feet wing_span=240.5 //Feet wing_root_chord=48.8 //Feet wing_dihedral=-1.0 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.81 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=29.0 //Degrees, wing leading edge wing_pos_apex_lon=16.5 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=10 //Feet, vertical distance from reference point, positive going up htail_area=2470 //Square feet htail_span=72.8 //Feet htail_pos_lon=-121.4 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=10.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=37.5 //Degrees, horizontal tail leading edge vtail_area=1660 //Square feet vtail_span=37.1 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-120.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up elevator_area=527 //Square feet aileron_area=325 //Square feet rudder_area=330 //Square feet elevator_up_limit=25 //Degrees elevator_down_limit=15 //Degrees aileron_up_limit=25 //Degrees aileron_down_limit=15 //Degrees rudder_limit=31.5 //Degrees elevator_trim_limit=20 //Degrees spoiler_limit=45 //Degrees spoiler_extension_time=2.0 //Seconds spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //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=130.0 //Knots True (KTAS) full_flaps_stall_speed=102.0 //Knots True (KTAS) cruise_speed=475.0 //Knots True (KTAS) max_mach=0.77 max_indicated_speed=365.0 //Red line (KIAS) [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 5 // degrees flaps-position.2 = 10 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 25 // degrees flaps-position.5 = 35 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.7 drag_scalar = 0.9 pitch_scalar= 0.9 system_type = 1 //Hydraulic [flaps.1] type = 2 // 1 - tail, 2 - lead span-outboard = 0.3 // 0.0 .. 1.0 extending-time = 15 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 6 // degrees flaps-position.2 = 12 // degrees flaps-position.3 = 18 // degrees flaps-position.4 = 24 // degrees flaps-position.5 = 30 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.3 drag_scalar = 0.1 pitch_scalar= 0.1 system_type = 1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=0.7 rudder_effectiveness=0.7 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=0.7 rudder_trim_effectiveness=0.7 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -2.0, -59.1, -2.6 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -18.4, -33.5, -4.3 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2 = -18.4, 33.5, -4.3 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3 = -2.0, 59.1, -2.6 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.17 //Scalar for fuel flow efficiency min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=77.2 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=50577 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? ThrustSpecificFuelConsumption=0.40 [jet_engine] thrust_scalar=1.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=95 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; 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=0.05 nav_proportional_control=16.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=18.0 gs_integrator_control=0.33 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=1.0 [contact_points] ;/0 Class <0=none,1=wheel, 2=scrape, 3=float> ;/1 Longitudinal Position (feet) ;/2 Lateral Position (feet) ;/3 Vertical Position (feet) ;/4 Impact Damage Threshold (Feet Per Minute) ;/5 Brake Map (0=None, 1=Left, 2=Right) ;/6 Wheel Radius (feet) ;/7 Steer Angle (degrees) ;/8 Static Compression (feet) (0 if rigid) ;/9 Max/Static Compression Ratio ;/10 Damping Ratio (0=Undamped, 1=Critically Damped) ;/11 Extension Time (seconds) ;/12 Retraction Time (seconds) ;/13 Sound Type ;/14 Airspeed limit for retraction (KIAS) ;/15 Airspeed that gear gets damage at (KIAS) point.0 = 1, 51.5, 0.0, -20.2, 1000.0, 0, 3.0, 70.0, 1.4, 1.0, 0.900, 12.0, 12.0, 0, 200, 230 point.1 = 1, -35.4, -13.5, -20.5, 3000.0, 1, 3.5, 13.0, 0.8, 2.0, 0.900, 15.0, 15.0, 2, 200, 230 point.2 = 1, -35.4, 13.5, -20.5, 3000.0, 2, 3.5, 13.0, 0.8, 2.0, 0.900, 15.0, 15.0, 3, 200, 230 point.3 = 2, 84.55, 0.0, -6.56, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.4 = 2, -39.43, 0.0, -17.13, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.5 = 2, -146.21, 0.0, 8.36, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.6 = 2, -52.78, -121.34, -5.12, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.7 = 2, -52.78, 121.34, -5.12, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.8 = 2, -142.61, -46.01, -5.12, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.9 = 2, -142.61, 46.01, -5.12, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 point.10 = 2, -138.88, 0.0, 50.06, 100.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch=-1.5 static_cg_height=18.6 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=5.0 //Flap angle that activates warning at idle flap_limit_power=25.5 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=1.24 //Brake scalar auto_brakes=4 hydraulic_system_scalar=1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,1,1 //pumps on Eng1,2,3,4 [Views] //eyepoint = 60.07, -1.97, 9.0 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) eyepoint = 60.07, -1.97, 9.1 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot=0, 5 , 17.0 avionics_bus=0, 5 , 17.0 avionics=1, 5 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 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 [Radios] ;/ Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing,6taxi,7reco,8wing,9logo,10cabin light.1 = 10, 60.07, 0.00, 8.80, fx_an124vc, light.2 = 1, 2.21, 0.00, 12.92, fx_an124beacon, light.3 = 1, 16.12, 0.00, -15.61, fx_an124beacon, light.4 = 5, 9.35, 45.41, -4.66, fx_an124land, light.5 = 5, 9.35, -45.41, -4.66, fx_an124land, light.6 = 5, 69.43, 0.00, -17.25, fx_an124land, light.7 = 9,-110.26, 10.79, 22.02, fx_an124logo , light.8 = 9,-110.26, -10.79, 22.02, fx_an124logo , [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 [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 [altimeters] altimeter.0=1 altimeter.1=1 [turn_indicators] ;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [vacuum_system] ;/Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi max_pressure=5.150000 vacuum_type=2 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [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 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 contrail=fx_contrail_l [exits] number_of_exits=4 exit.0=0.4, 46.05, -12.50, -6.79, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1=0.4, -146.0, 8.0, -7.5, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2=0.4, -42.30, 9.0, -7, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.3=0.04, -70.41, 6.0, -12.80, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 stick_shaker=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [smokesystem] smoke.0 = -38, -69.5, -6.9, fx_engsmoke smoke.1 = -22.0, -38.9, -10.4, fx_engsmoke smoke.2 = -22.0, 38.9, -10.4, fx_engsmoke smoke.3 = -38.5, 69.5, -6.9, fx_engsmoke