[fltsim.0] title=b727 sim=b727 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=N72720 atc_airline=American Airlines atc_flight_number=A9286 ui_manufacturer=Boeing ui_type="727-200" ui_variation="American Airlines" description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. [fltsim.1] title=b727 Paint1 sim=b727 model= panel= sound= texture=1 kb_checklists= kb_reference= atc_id=N2812W atc_airline=Viasa atc_flight_number=A9265 ui_manufacturer=Boeing ui_type="727-200" ui_variation="Viasa" description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. [fltsim.2] title=b727 Paint2 sim=b727 model= panel= sound= texture=2 kb_checklists= kb_reference= atc_id=N2812W atc_airline=Northwest atc_flight_number=A9265 ui_manufacturer=Boeing ui_type="727-200" ui_variation="Northwest" description=The 727-200 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. [fltsim.3] title=b727 Paint3 sim=b727 model= panel= sound= texture=3 kb_checklists= kb_reference= atc_id=N2812W atc_airline=Lufthansa atc_flight_number=2184 ui_manufacturer=Boeing ui_type="727-200" ui_variation="Lufthansa" description=The 727-200 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. [fltsim.4] title=b727 Paint4 sim=b727 model= panel= sound= texture=4 kb_checklists= kb_reference= atc_id=N72720 atc_airline=Northwest atc_flight_number=2184 ui_manufacturer=Boeing ui_type="727-200" ui_variation="Northwest" description=The 727-100 had been in service barely a year when Boeing began serious consideration of a stretched, greater capacity development.This resulted in the 727-200, which Boeing announced it was developing in August 1965. The 727-200 was essentially a minimum change development of the 100, the only major change being the 6.10m (20ft) fuselage stretch, which increased maximum seating to 189 passengers. The 727-200's stretch consisted of two 3.05m (10ft) plugs, one forward and one rear of the wing. Otherwise the 727-100 and 200 shared common engines, fuel tank capacity and the same maximum takeoff weight.The first flight of the 727-200 occurred on July 27 1967, with certification granted in late November that year. The -200 was placed into service by launch customer Northeast Airlines (this airline was later acquired by Delta) the following month, by which time total 727 orders for both models had exceeded 500.The 727-200 helped broaden the sales appeal of the 727 considerably and snared significant sales. Category = airplane [CameraDefinition.0] Title = "Right Side Window" Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC} Description = View of the right wing from the passenger cabin 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 = "Left Side Window" Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a} Description = View of the left wing from the passenger cabin 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 = "Landing Gear" Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051} Description = View of the landing gear and left wing inboard flaps 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 = "Tail" Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c} Description = Looking forward from behind the aircraft 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 = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the 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 = "Left Wing" Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de} Description = View from the left wing tip looking at the 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 = "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 = .6 SmoothZoomTime = 2.0 ZoomPanScalar = 0.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.50, 0.0, 0.0 InitialPbh=2, 0, 0 [CameraDefinition.002] Title = "Center Console" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 SmoothZoomTime = 2.0 ZoomPanScalar = 2.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.45, 0.30, -0.15 InitialPbh=84.2, 0, 0 [CameraDefinition.003] Title = "Engine Controls" Guid = {a5741a54-ea6d-4580-9709-c99161e38a83} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.45, 0.10, 0.35 InitialPbh=85.0, 0, 0 [CameraDefinition.004] Title = "Overhead Panel" Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.7 SmoothZoomTime = 2.0 ZoomPanScalar = 1.15 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.47, -0.62, -0.4 InitialPbh=-58.0, 0, 0 [General] atc_type=BOEING atc_model=B722 editable=0 performance=Cruise Speed: FL280-390\nMaximum Range: 1,810 nm\nService Ceiling: 39,000 ft\nEmpty Weight: 97,770 lbs\nFuel Weight: 54,203 lbs (8,090 US Gal) \nMax Takeoff Weight: 190,500 lbs\nMax Landing Weight: 161,000 lbs\nVmo\/Mmo: 375kts\/M0.91\n ( FL100\/Mach)\nClimb: 250kts\/300kts\/M0.76\nMax Cruise: 250kts\/350kts\/M0.82\nDescent: 250kts\/280kts\/M0.77 Category=airplane [pitot_static] vertical_speed_time_constant=50 pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight=190500 empty_weight=97770 reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=1.826, 0.000, 1.908 max_number_of_stations=8 station_load.0= "190.0, 68.170, -1.206, 4.683, Pilot" station_load.1 = "190.0, 68.170, 1.206, 4.683, First Officer" station_load.2 = "190.0, 64.527, 0.000, 4.683, Flt Engineer" station_load.3 = "260.0, 60.191, -1.895, 4.683, 2-Flt Attendant" station_load.4 ="33150.0, 16.652, 0.000, 4.683, 170-Coach Pax" station_load.5 = "260.0, -28.794, 0.000, 4.683, 2-Flt Attendant" station_load.6 = "1187.2, 33.998, 0.000, -0.347, Forward Cargo" station_load.7= "1362.8, -16.826, 0.000, -0.347, Aft Cargo" ;Moments of Inertia empty_weight_pitch_MOI=10000000 empty_weight_roll_MOI=5000000 empty_weight_yaw_MOI=9300000 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 [GeneralEngineData] engine_type=1 Engine.0=-43.018, -8.958, 5.551 Engine.1 =-60.711, 0.000, 5.030 Engine.2=-43.018, 8.958, 5.551 fuel_flow_scalar=1.941 min_throttle_limit=-0.500 max_contrail_temperature=-30 [SMOKESYSTEM] smoke.0=5.551, -58.018,-8.958, smoke_jt8d smoke.1=5.030, -75.711, 0.000, smoke_jt8d smoke.2=5.551, -58.018, 8.958, smoke_jt8d [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=9.852 rated_N2_rpm=12250.000 static_thrust=17400.000 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.000 [electrical] max_battery_voltage=28 generator_alternator_voltage=28 max_generator_alternator_amps=60 engine_generator_map=1,1,1 electric_always_available=1 autopilot=0, 5, 17 avionics_bus=0, 10, 17 avionics=1, 5, 17 pitot_heat=0, 15, 17 additional_system=0, 20, 17 marker_beacon=1, 2, 17 gear_warning=0, 2, 17 fuel_pump=0, 5, 17 starter1=0, 20, 17 starter2=0, 20, 17 starter3=0, 20, 17 light_nav=0, 5, 17 light_beacon=0, 5, 17 light_landing=0, 5, 17 light_taxi=0, 5, 17 light_strobe=0, 5, 17 light_panel=0, 5, 17 auto_brakes=0, 15, 17 hydraulic_pump=0, 2, 17 fuel_transfer_pump=0, 5, 17 //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=1.000, 60.648, 0.000, -7.800, 1056.000, 0.000, 1.333, 50.000, 0.500, 3.500, 0.750, 8.000, 8.000, 0.000, 0.000, 270.000 point.1=1.000, -2.602, -9.375, -8.350, 1320.000, 1.000, 2.083, 0.000, 0.500, 4.500, 0.990, 8.200, 8.200, 2.000, 0.000, 270.000 point.2=1.000, -2.602, 9.375, -8.350, 1320.000, 2.000, 2.083, 0.000, 0.500, 4.500, 0.990, 8.200, 8.200, 3.000, 0.000, 270.000 point.3=2.000, 63.140, 0.000, -2.775, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.4=2.000, 0.000, 0.000, -3.469, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.5=2.000, -35.386, 0.000, -1.387, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6=2.000, -21.189, -52.715, 0.688, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.7=2.000, -21.189, 52.715, 0.688, 60.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 max_number_of_points=8 static_pitch=-1.110 static_cg_height=8.300 gear_system_type=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.050 flap_limit_idle=15.5 flap_limit_power=25.5 [brakes] parking_brake=1 toe_brakes_scale=0.550 auto_brakes=4 [hydraulic_system] normal_pressure=3000.0 electric_pumps=0 engine_map=1,1,1,0 [Views] eyepoint=68.170, -1.206, 5.898 [Flaps.0] //Sets initial trailing drag, lift, and visuals type=1 span-outboard=0.800 extending-time=30.000 flaps-position.0=0.000 flaps-position.1=2.000 flaps-position.2=5.000 flaps-position.3=15.000 flaps-position.4=20.000 flaps-position.5=25.000 flaps-position.6=30.000 flaps-position.7=40.000 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.500 drag_scalar=0.200 pitch_scalar=0.000 system_type=1 [Flaps.1] //Adjusts trailing drag factors type=1 span-outboard=0.800 extending-time=30.000 flaps-position.0=0.000 flaps-position.1=4.435 flaps-position.2=2.779 flaps-position.3=10.623 flaps-position.4=25.389 flaps-position.5=48.874 flaps-position.6=91.302 flaps-position.7=185.320 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.000 drag_scalar=0.200 pitch_scalar=0.000 system_type=1 [Flaps.2] //Adjusts trailing lift factors type=1 span-outboard=0.800 extending-time=30.000 lift_scalar=0.800 drag_scalar=0.000 pitch_scalar=0.000 flaps-position.0=0.000 flaps-position.1=5.900 flaps-position.2=5.750 flaps-position.3=4.783 flaps-position.4=8.762 flaps-position.5=11.003 flaps-position.6=14.831 flaps-position.7=22.851 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.500 drag_scalar=0.000 pitch_scalar=0.000 system_type=1 [Flaps.3] //Sets leading visual graphics type=2 span-outboard=0.800 extending-time=6.000 flaps-position.0=0.000, 0.000 flaps-position.1=1.000, 0.000 flaps-position.2=2.000, 0.000 damaging-speed=250.000 blowout-speed=300.000 lift_scalar=0.000 drag_scalar=0.000 pitch_scalar=0.000 system_type=1 [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 light.0=1, 8.00, 0.00, -3.65, fx_beaconb , light.1=1, 27.70, 0.00, 11.40, fx_beaconh, light.2=2, -30.00, -60.01, 2.30, fx_strobeh , light.3=2, -30.00, 60.00, 2.30, fx_strobeh , light.4=2, -96.70, 0.00, 24.60, fx_strobe , light.5=3, -96.70, 0.00, 24.60, fx_navwhi , light.6=3, -30.00, -60.1, 2.30, fx_navredm , light.7=3, -30.00, 60.0, 2.30, fx_navgrem //light.8=4, 68.60, 2.00, 4.50, fx_vclighth , light.9=4, 68.60,-0.50, 4.50, fx_vclighth , light.10=4, 64.60,-2.50, 5.50, fx_vclight , //light.11=4, 64.60, 2.00, 5.50, fx_vclight , [keyboard_response] elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] direction_indicator.0=2 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0 [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 visual_damage=1 //windshield_rain_effect_available = 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=100 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=99 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 max_pitch=10.0 max_pitch_acceleration=1.5 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=1.00 default_pitch_mode=0 default_bank_mode=0 [fuel] //8090 US Gallons Total Center1=10.851, 0.000, -0.520, 4530.000, 0.000 LeftMain=5.685, -16.710, 0.000, 1780.000, 0.000 RightMain=5.685, 16.710, 0.000, 1780.000, 0.000 fuel_type=2 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1650.000 wing_span=108.000 wing_root_chord=25.151 wing_dihedral=3.000 wing_incidence=2.000 wing_twist=-0.500 oswald_efficiency_factor=0.800 wing_winglets_flag=0 wing_sweep=32.000 wing_pos_apex_lon=24.118 wing_pos_apex_vert=0.867 htail_area=376.000 htail_span=35.761 htail_pos_lon=-55.471 htail_pos_vert=24.284 htail_incidence=0.000 htail_sweep=42.000 vtail_area=290.000 vtail_span=15.092 vtail_sweep=57.000 vtail_pos_lon=-32.784 vtail_pos_vert=10.755 elevator_area=107.996 aileron_area=67.404 rudder_area=66.171 elevator_up_limit=27.000 elevator_down_limit=17.000 aileron_up_limit=17.000 aileron_down_limit=17.000 rudder_limit=25.000 elevator_trim_limit=9.500 spoiler_limit=60.000 spoilerons_available=1 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=10.000 min_flaps_for_spoilerons=0.000 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=146.000 full_flaps_stall_speed=122.000 cruise_speed=488.000 max_mach=0.910 max_indicated_speed=375.000 [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