[fltsim.0] title=Vista Liners Boeing 737-300 Lufthansa D-ABXL Neuss sim=B737_300 model= panel= sound= texture=lufthansaxl visual_damage=1 kb_checklists=Boeing737-800_check kb_reference=Boeing737-800_ref atc_id=D-ABXL atc_airline=Lufthansa atc_flight_number=081 ui_manufacturer=Boeing ui_type=737-300 ui_variation=Lufthansa D-ABXL 'Neuss' description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service. [CameraDefinition.0] Title=Rechtes Seitenfenster Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description=Ansicht der rechten Tragfläche aus der Passagierkabine Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.8 ShowWeather=Yes InitialXyz=3.2, 1.8, -5 InitialPbh=5, 0, 100 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title=Linkes Seitenfenster Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description=Ansicht der linken Tragfläche aus der Passagierkabine Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.8 ShowWeather=Yes InitialXyz=-3.2, 1.8, -5 InitialPbh=5, 0, 260 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.2] Title=Fahrwerk Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description=Ansicht des Fahrwerks und der Innenklappen der linken Tragfläche Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.52 ShowWeather=Yes InitialXyz=-3.3, -1.8, -11 InitialPbh=0, 0, 17 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.3] Title=Heck Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c} Description=Ansicht nach vorn von einer Position hinter dem Luftfahrzeug Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=.75 ShowWeather=Yes InitialXyz=0, 6.5, -55.0 InitialPbh=5, 0, 0 XyzAdjust=TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.4] Title=Rechte Tragfläche Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59} Description=Ansicht von der rechten Tragflächenspitze in Richtung Cockpit Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=30.8, 1.6, 4.0 InitialPbh=6, 0, 270 XyzAdjust=TRUE Category=Aircraft MomentumEffect=FALSE ClipMode=Minimum [CameraDefinition.5] Title=Linke Tragfläche Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description=Ansicht von der linken Tragflächenspitze in Richtung Cockpit Origin=Center SnapPbhAdjust=Swivel SnapPbhReturn=FALSE PanPbhAdjust=Swivel PanPbhReturn=FALSE Track=None ShowAxis=FALSE AllowZoom=TRUE InitialZoom=0.5 ShowWeather=Yes InitialXyz=-30.8, 1.6, 4.0 InitialPbh=6, 0, 90 XyzAdjust=TRUE Category=Aircraft MomentumEffect=No ClipMode=Minimum [CameraDefinition.001] Title=Rechter Sitz 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=.6 SmoothZoomTime=2.0 ZoomPanScalar=1.0 ShowWeather=Yes XyzAdjust=TRUE ShowLensFlare=FALSE Category=Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.94, 0.0, 0.0 InitialPbh=2, 0, 0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -12.5, -50.8, 1.9, fx_navred light.1 = 3, -12.9, -50.8, 1.9, fx_navred light.2 = 3, -12.5, 50.8, 1.9, fx_navgre light.3 = 3, -12.9, 50.8, 1.9, fx_navgre light.4 = 3, -17.2, 50.65, 1.9, fx_navwhi light.5 = 3, -17.2, -50.65, 1.9, fx_navwhi light.6 = 2, -13, -50.8, 1.9, fx_strobe light.7 = 2, -13, 50.8, 1.9, fx_strobe light.8 = 2, -57.4, 0.00, 6.4, fx_strobe , light.9 = 3, -57.4, 0.00, 6.4, fx_navwhi , light.10 = 1, 7.1, 0, 9.6, fx_beaconb light.11 = 1, 5.50, 0.00, -4.90, fx_beaconh, light.12 = 4, 44.0000, 0.00, 2.2, fx_vclighth , [contact_points] point.0=1.000, 41.447, 0.000, -8.832, 1181.1, 0, 1.442, 78.0, 0.6, 1.372, 0.9, 4.0, 4.0, 0, 220.0, 250.0 point.1=1.000, -9.410, -9.919, -9.827, 1574.8, 1, 1.442, 0.00, 1.0, 1.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0 point.2=1.000, -9.410, 9.919 -9.827, 1574.8, 2, 1.442, 0.00, 1.0, 1.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0 point.3=2.000, 42.747, 0.000, 4.243, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Nose scrape point.4=2.000, -33.316, 0.000, 2.421, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Tail scrape point.5=2.000, -13.585, -50.333, 2.08, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Left wing scrape point.6=2.000, -13.585, 50.333, 2.08, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Right wing scrape static_pitch=-0.900000 static_cg_height=9.919 gear_system_type=0 [Views] eyepoint=34.129659,-1.307210,3.614050 [exits] number_of_exits=2 exit_rate.0 = 0.28 exit_rate.1 = 0.28 [TailHook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=0.7 [folding_wings] wing_fold_system_type=4 fold_rates=0.12,0.11 //////////////////////////////// [GeneralEngineData] engine_type = 1 Engine.0 = 4.75, -16.1, -4.5 Engine.1 = 4.75, 16.1, -4.5 fuel_flow_scalar = 1 min_throttle_limit = -0.25 max_contrail_temperature = -30 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 19.6 rated_N2_rpm = 29920 static_thrust = 18920 /CFM56-3B2 @ 22,000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar = 1.0 //////////////////////////////// [General] atc_type=BOEING atc_model=B733 editable=0 performance="Cruise Speed \n477 kts 550 mph 885 km\/h\n\nEngines \nCFM56-3C1\n\nMaximum Range \n2,059 nm 2,370 mi 3,810 km\n\nService Ceiling \n36, 089 ft 11,000 m\n\nFuel Capacity \n5,311 U.S. gal 20,104 L\n\nEmpty Weight-Standard \n76,180 lb 34,550 kg\n\nMaximum Gross Weight\n150,000 lb 68,039 kg\n\nLength \n120 ft 36.45 m\n\nWingspan \n94 ft, 9 in 25.9 m\n\nHeight \n36.5 ft 11.13 m\n\nSeating \nSeats 147 to 168\n\nCargo Capacity \n1,373 ft3 38.93 m3\n\n" Category=airplane [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight = 150000 // (pounds) empty_weight = 74170 // (pounds) reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -5, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 3172439 empty_weight_roll_MOI = 2262183 empty_weight_yaw_MOI = 3337024 empty_weight_coupled_MOI = 0 [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 [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 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 5.0 flap_limit_power = 25.5 [brakes] parking_brake = 1 toe_brakes_scale = 0.885 auto_brakes=4 [hydraulic_system] normal_pressure = 3000.0 electric_pumps = 0 engine_map = 1,1,0,0 [flaps.0] //Trailing Edge Flaps 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 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 15 // degrees flaps-position.6 = 25 // degrees flaps-position.7 = 30 // degrees flaps-position.8 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.1] //Inboard Leading Edge Flaps type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // flaps-position.1 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 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 [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=0,0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 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=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [fuel] Center1 = 0, 0, 0, 2313, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -3, -19, 0, 1500, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -3, 19, 0, 1500, 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=0 [airplane_geometry] wing_area = 1137.0 //Square feet wing_span = 94.75 //Feet wing_root_chord = 18.0 //Feet wing_dihedral = 6.2 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -0.5 //Degrees oswald_efficiency_factor= 0.75 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 25.0 //Degrees, wing leading edge wing_pos_apex_lon = 8.0 //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 = 338.0 //Square feet htail_span = 41.7 //Feet htail_pos_lon = -35.0 //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 = 0.0 //Degrees htail_sweep = 30.0 //Degrees, horizontal tail leading edge vtail_area = 224.0 //Square feet vtail_span = 20.0 //Feet, tip to body vtail_sweep = 35.0 //Degrees, vertical tail leading edge vtail_pos_lon = -35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up elevator_area = 70.5 //Square feet aileron_area = 26.9 //Square feet rudder_area = 56.2 //Square feet elevator_up_limit = 22.5 //Degrees elevator_down_limit = 19.5 //Degrees aileron_up_limit = 20.0 //Degrees aileron_down_limit = 20.0 //Degrees rudder_limit = 26.0 //Degrees elevator_trim_limit = 20.0 //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 [Reference Speeds] flaps_up_stall_speed = 142.0 //Knots True (KTAS) full_flaps_stall_speed = 113.0 //Knots True (KTAS) cruise_speed = 477.0 //Knots True (KTAS) max_mach = 0.82 max_indicated_speed = 340 //Red line (KIAS) [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 [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=1.000000 [deice_system] structural_deice_type=0