[fltsim.0] title=Eastern_gray A300-B4 sim=TomA300b model=4GEnew panel=A300B4GE sound= texture=Eastern kb_checklists= kb_reference= atc_id=N204EA atc_airline=Eastern atc_flight_number=1157 atc_heavy=1 ui_manufacturer=Airbus ui_typerole=Commercial Airliner ui_createdby=Thomas Ruth ui_type=A300-B4 ui_variation=EASTERN A300-B4 [fltsim.1] title=Eastern_OC A300-B4 sim=TomA300b model=4GEold panel=A300B4GE sound= texture=Eastern_OC kb_checklists= kb_reference= atc_id=N204EA atc_airline=Airbus atc_flight_number=1424 atc_heavy=1 ui_manufacturer=Airbus ui_typerole=Commercial Airliner ui_createdby=Thomas Ruth ui_type=A300-B4 ui_variation=EASTERN A300-B4 OC [General] atc_type=AIRBUS atc_model=A3B4 editable=1 performance="Reisegeschwindigkeit\nMach 0.78 515 mph 829 kmh\n\nTriebwerkoption \nP&W 4158\CF6-80C2\n\nMaximale Reichweite \n4.070 nm 7.540 km\n\nDienstgipfelhöhe \n42.000 Fuß 12.800 m\n\nTreibstoffmenge \n18.000 Gallonen 68.150 L \n\nMaximales Startgewicht \n375.100 lbs 170.500 kg\n\nLänge \n177 Fuß, 3 Zoll 54.08 m\n\nSpannweite \n147 Fuß, 2 Zoll 44.85 m\n\nHöhe \n54 Fuß, 6 Zoll 16.62 m\n\nSitzplätze \nca 266 \n\nFrachtkapazität \n147.4 Kubikmeter\n" Category=airplane [CameraDefinition.0] Title=Left wingview Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description=Left trailing edge as seen from paxcabin Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.4 ShowWeather=Yes InitialXyz=-2.118, 1.067, 3.665 InitialPbh=5, 0, 260 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title=Right wingview Guid={D368D3EA-21FB-4d88-97BC-771106DCC59B} Description=Right trailing edge as seen from paxcabin Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.4 ShowWeather=Yes InitialXyz=2.018, 1.167, -4.465 InitialPbh=5, 0, 80 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE 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=.5 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=1.0, 0.5, -0.7 InitialPbh=0, 0, 0 [CameraDefinition.002] Title=Jump Seat 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=.7 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=-0.43, 0.50, -1.2 InitialPbh=0, 0, 0 [CameraDefinition.003] Title=Flight Engineer Guid={5CBF7C35-60CA-4e72-9B9F-4E7C89BAC621} Origin=Virtual Cockpit MomentumEffect=YES SnapPbhAdjust=Swivel SnapPbhReturn=False PanPbhAdjust=Swivel PanPbhReturn=False Track=None ShowAxis=YES AllowZoom=TRUE InitialZoom=.7 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.83, 0.00, -1.11 InitialPbh=0, 0, 90 [WEIGHT_AND_BALANCE] max_gross_weight = 363763 // (pounds) empty_weight = 194404 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170.0, 86.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170.0, 86.0, 2.0, 0.0, Kopilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "850.0, 0.0, 0.0, 0.0, Besatzung" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "850.0, 52.0, 0.0, 0.0, Erste Klasse (PAX only)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "1870.0, 11.0, 0.0, 0.0, Businessklasse (Pax only)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "2740.0, -30.0, 0.0, 0.0, Sitz 1-16 / Cargo Front" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "1550.0, -72.5, 0.0, 0.0, Sitz 16-29 / Cargo Aft" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "1800.0, 47.0, 0.0, -6.0, Fracht vorne" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "500.0, -67.0, 0.0, -6.0, Fracht hinten" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 7000000 empty_weight_roll_MOI = 10500000 empty_weight_yaw_MOI = 6300000 empty_weight_coupled_MOI= 0.0 CG_forward_limit = 0.000 CG_aft_limit = 1.000 [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 = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 0.33, -25.98, -8.56 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = 0.33, 25.98, -8.56 //(feet) longitudinal, lateral, vertical distance from reference datum //fuel_flow_scalar = 1.0 ORIGINAL fuel_flow_scalar = 1.00 //Scalar for fuel flow efficiency min_throttle_limit = -0.25; //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature=-30 [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 90.0 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 52500 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=30.0 max_generator_alternator_amps=400.0 ;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 light_logo = 0, 5 , 17.0 light_wing = 0, 5 , 17.0 //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] point.0=1, 55.77, 0.00, -15.95, 1181.1, 0, 1.669, 90.0, 0.4921, 2.7667, 0.7235, 4.0, 4.0, 0, 270.0, 270.0 point.1=1, -8.17, -14.73, -16.53, 1574.8, 1, 2.064, 0.0, 0.4921, 2.6401, 0.7470, 6.9, 6.9, 2, 270.0, 270.0 point.2=1, -8.17, 14.73, -16.53, 1574.8, 2, 2.064, 0.0, 0.4921, 2.6401, 0.7470, 7.1, 7.1, 3, 270.0, 270.0 point.3=2, -26.30, -73.64, 2.89, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -26.30, 73.64, 2.89, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -96.67, 0.00, 6.18, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 79.24, 0.00, -0.35, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = 0.10 static_cg_height = 17.00 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 = 1.0 //Brake scalar auto_brakes=5 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 = 1 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] //eyepoint = 69.66, -1.43, 3.65 eyepoint = 68.89, -1.90, 3.60 //A300 = 69.90, -1.77, 3.77 [flaps.0] //Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.2 // 0.0 .. 1.0 extending-time = 25 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 3 // degrees flaps-position.2 = 15 // degrees flaps-position.3 = 20 // degrees flaps-position.4 = 26 // degrees flaps-position.5 = 35 // degrees damaging-speed = 220 // KIAS blowout-speed = 260 // KIAS lift_scalar = 0.547 //0.57 drag_scalar = 1.25 pitch_scalar = 0 system_type = 1 //Hydraulic [flaps.1] //Leading Edge type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 23 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 18 // degrees flaps-position.2 = 18 // degrees flaps-position.3 = 22 // degrees flaps-position.4 = 22 // degrees flaps-position.5 = 27 // degrees damaging-speed = 250 // KIAS blowout-speed = 270 // KIAS lift_scalar = 0.5 //0.55 drag_scalar = 0.4 pitch_scalar = 0.2 system_type = 1 //Hydraulic [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 [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 [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 [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] max_pressure=5.15 // PSI vacuum_type=2 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi [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 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing,6taxi,7reco,8wing,9logo,10cabin light.0 = 1, 15.95, 0.00, 9.94, fx_T332beacon , light.1 = 1, 9.81, 0.00, -9.22, fx_T332beacon , light.2 = 5, 16.13, 9.28, -2.27, fx_T332land , light.3 = 5, 16.13, -9.28, -2.27, fx_T332land , light.4 = 9, -84.01, 4.59, 14.82, fx_T332logo , light.5 = 9, -84.01, -4.59, 14.82, fx_T332logo , light.6 = 10, 67.92, 0.00, 3.00, fx_vclighth , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits = 4 exit.0 = 0.4, 58.57, -7.12, 2.8, 0 ;Percent per second exit.1 = 0.04, -46.13, 7.50, -5.59, 1 ;Percent per second exit.2 = 0.4, -28.803, -8.540, -3.868, 2 ;Percent per second exit.3 = 0.4, -28.803, -8.540, -3.868, 2 ;Percent per second [fuel] Center1 = 4.4, 0.0, -5.4, 4646.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = 2.99, -31.7, 0, 4420.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = 2.99, 31.7, 0, 4420.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux = -16.6, -57.6, 1.8, 1260.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux = -16.6, 57.6, 1.8, 1260.0, 3.0 //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=0.0087 //Percent of max quantity per second, i.e. about 1 minute for full fuel [airplane_geometry] wing_area = 2893.0 //Square feet wing_span = 147.2 //Feet wing_root_chord = 35.1 //Feet wing_dihedral = 5.5 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.72 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 28.0 //Degrees, wing leading edge wing_pos_apex_lon = 20.0 //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 = 716.9 //Square feet htail_span = 63.16 //Feet htail_pos_lon = -98.07 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 5.87 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 34.0 //Degrees, horizontal tail leading edge vtail_area = 560.0 //Square feet vtail_span = 30.84 //Feet, tip to body vtail_sweep = 39.0 //Degrees, vertical tail leading edge vtail_pos_lon = -97.74 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 25.6 //Feet, vertical distance from reference point, positive going up elevator_area = 75.9 //Square feet aileron_area = 48.0 //Square feet rudder_area = 126.0 //Square feet elevator_up_limit = 30.0 //Degrees elevator_down_limit = 15.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 15.0 //Degrees rudder_limit = 25.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 60.0 //Degrees 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 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 //fly_by_wire=1 [Reference Speeds] flaps_up_stall_speed = 150.0 //Knots True (KTAS) full_flaps_stall_speed = 120.0 //Knots True (KTAS) cruise_speed = 447.0 //Knots True (KTAS) max_mach = 0.82 max_indicated_speed = 340 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1500.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm = 90 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=0.10 nav_proportional_control=11.00 nav_integrator_control=0.17 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=19.0 gs_integrator_control=0.530 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [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 [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9