[fltsim.0] title=Boeing 747-281B Northwest Airlines Cargo (Project Opensky) sim=Boeing747-200B-GE-CF6-50E2 model= panel= sound= texture= checklists= atc_airline=Northwest atc_id=N616US atc_flight_number=4156 atc_heavy=1 ui_manufacturer=Boeing ui_type=747-200 ui_variation=Northwest Cargo visual_damage=1 description=Project Opensky \nBoeing 747-200B\nVersion 2002.3.1\n\nEngine Type GE CF6-50E2\n\n747-200 Commercial Version \n\nModel Designers\n Mitsushi Yutaka\n Hiroshi Igami \n\nFlight Dynamics Designer\n Warren C. Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo Kitaguchi\n\nTest Pilots\n Repaint by Tony Radmilovich\n\n\nMaximun Range: 6,370 nm\n\nTypical city pairs: \n Tokyo-NY\n Bangkok-Paris\n London-Johannesburg\n\nFor proper operation: See B747 manual at: \n www.project-opensky.com [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=2.0 aileron_effectiveness=2.0 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 [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 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=538340.000000 empty_weight_roll_MOI=11331310.000 empty_weight_pitch_MOI=36732189.000 empty_weight_yaw_MOI=32844259.000 empty_weight_coupled_MOI=1000.000 max_gross_weight=833000.00 CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] Center1=0.000, 0.0, -4.0, 17153.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) //Center2=-193.5, 0.0, 6.0, 3298.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-5.0, -35.0, -4.0, 12538.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-11.5, -52.0, -3.0, 5761.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-5.0, 35.0, -4.0, 12538.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-11.5, 52.0, -3.0, 5761.0, 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 [airplane_geometry] wing_area=5500.000 wing_span=196.000 wing_root_chord=23.000 wing_dihedral=6.998 wing_incidence=2.000 wing_twist=-0.994 oswald_efficiency_factor=0.830 wing_winglets_flag=0 wing_sweep=37.500 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=1470.000 htail_span=72.750 htail_pos_lon=-17.167 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=37.500 vtail_area=1060.000 vtail_span=37.121 vtail_sweep=45.000 vtail_pos_lon=-16.500 vtail_pos_vert=6.083 elevator_area=326.800 aileron_area=225.200 rudder_area=229.900 elevator_up_limit=13.751 elevator_down_limit=10.313 aileron_up_limit=31.513 aileron_down_limit=31.513 rudder_limit=17.189 elevator_trim_limit=9.167 spoiler_limit=25.783 spoilerons_available=0 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=11.459 min_flaps_for_spoilerons=0.000 [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=1.000, 67.333, 0.000, -13.850, 1181.102, 0.000, 5.812, 78.480, 0.859, 0.500, 0.518, 11.000, 11.000, 0.000, 0.000, 0.000 point.1=1.000, -12.583, -18.000, -13.833, 1574.803, 1.000, 5.812, 0.000, 0.602, 0.500, 0.551, 14.900, 14.900, 2.000, 0.000, 0.000 point.2=1.000, -12.583, 18.000, -13.833, 1574.803, 2.000, 5.812, 0.000, 0.602, 0.500, 0.551, 17.100, 17.100, 3.000, 0.000, 0.000 point.3=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -14.167, 96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, -132.667, 0.000, 2.500, 787.402, 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, 88.167, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8=2.000, -132.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch=-1.000 static_cg_height=13.625 // Nose gear //point.0=1.000, 67.333, -1.500, -14.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000 //point.1=1.000, 67.333, 1.500, -14.333, 1181.102, 0.000, 2.000, 70.000, 1.859, 2.500, 0.518, 9.000, 11.000, 0.000, 240.000, 280.000 // // Main Wing Gear (left) //point.2=1.000, -7.583, -18.000, -15.833, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000 //point.3=1.000, -7.583, -14.000, -15.833, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000 //point.4=1.000, -2.583, -18.000, -15.833, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000 //point.5=1.000, -2.583, -14.000, -15.833, 1574.803, 1.000, 2.000, -13.000, 2.602, 2.500, 0.551, 12.900, 14.900, 2.000, 240.000, 280.000 // Main Wing Gear (right) //point.6=1.000, -7.583, 18.000, -15.833, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000 //point.7=1.000, -7.583, 14.000, -15.833, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000 //point.8=1.000, -2.583, 18.000, -15.833, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000 //point.9=1.000, -2.583, 14.000, -15.833, 1574.803, 2.000, 2.000, -13.000, 2.602, 2.500, 0.551, 15.100, 16.400, 3.000, 240.000, 280.000 // Main Center Gear (left) //point.10=1.000, -18.583, -8.000, -15.833, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000 //point.11=1.000, -18.583, -4.000, -15.833, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000 //point.12=1.000, -12.583, -8.000, -15.833, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000 //point.13=1.000, -12.583, -4.000, -15.833, 1574.803, 1.000, 2.000, 0.000, 2.602, 2.500, 0.551, 13.400, 14.900, 2.000, 240.000, 280.000 // Main Center Gear (right) //point.14=1.000, -18.583, 8.000, -15.833, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000 //point.15=1.000, -18.583, 4.000, -15.833, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000 //point.16=1.000, -12.583, 8.000, -15.833, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000 //point.17=1.000, -12.583, 4.000, -15.833, 1574.803, 2.000, 2.000, 0.000, 2.602, 2.500, 0.551, 11.500, 17.500, 3.000, 240.000, 280.000 // //Scrape points //point.18=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //point.19=2.000, -14.167, 96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //point.20=2.000, -132.667, 0.000, 2.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //point.21=2.000, 88.167, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //point.22=2.000, -14.167, -96.167, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 //point.23=2.000, -132.667, 0.000, 55.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // //static_pitch=-1.000 //static_cg_height=13.625 [GeneralEngineData] engine_type=1 Engine.0=-14.916667,-69.500000,0.000000 Engine.1=14.916667,-39.166667,-7.000000 Engine.2=14.916667,39.166667,-7.000000 Engine.3=-14.916667,69.500000,0.000000 fuel_flow_scalar=0.8676 [TurbineEngineData] bypass_ratio=4.970000 fuel_flow_gain=0.001000 inlet_area=37.558941 rated_N2_rpm=26928.000000 static_thrust=52500.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=150.000 full_flaps_stall_speed=126.000 cruise_speed=424.337 [keyboard_response] elevator=100.000, 200.000 aileron=100.000, 200.000 rudder=150.000, 250.000 [Views] eyepoint=77.330, -1.487, 20.005 [General] performance=Passengers\n3-class conf: 366 \n2-class conf: 452 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3) \n\nDimensions\nSpan 195 ft 8 in\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: GE CF6-50E2\nTO Thrust: 52,500 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 538,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 6,370 nm\nTypical Cruise Speed \n @ FL350: M.84 atc_type=BOEING AIRCRAFT atc_model=B742 editable=0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=105.000 pitch_takeoff_ga=8.000 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=5 // degrees flaps-position.2=10 // degrees flaps-position.3=15 // degrees flaps-position.4=20 // degrees flaps-position.5=25 // degrees flaps-position.6=30 // degrees damaging-speed=200 // KIAS blowout-speed=250 // KIAS lift_scalar=0.7 drag_scalar=1.0 pitch_scalar=0.9 system_type=1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=12 // seconds flaps-position.0=0 // degrees flaps-position.1=20.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.3 drag_scalar=1.0 pitch_scalar=0.1 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [direction_indicators] direction_indicator.0=3,0 [electrical] // ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=1, 0 , 1.0 gear_motor=0, 5 , 17.0 avionics_bus=0, 0 , 1.0 avionics=1, 5 , 17.0 pitot_heat=0, 0 , 1.0 additional_system=0, 0 , 1.0 marker_beacon=1, 2 , 17.0 gear_warning=7, 0 , 99.0 gear_motor=4, 0 , 1.0 fuel_pump=0, 0 , 1.0 fuel_transfer_pump=0, 0 , 1.0 starter1=0, 20, 17.0 starter2=0, 0 , 1.0 light_nav=0, 0 , 1.0 light_beacon=0, 0 , 1.0 light_landing=0, 0 , 1.0 light_taxi=0, 0 , 1.0 light_strobe=0, 0 , 1.0 light_panel=0, 7 , 99.0 light_recognition=0, 0 , 1.0 light_wing=0, 0 , 1.0 marker_beacon=0, 0 , 1.0 standby_vacuum=0, 0 , 1.0 auto_brakes=0, 0 , 1.0 hydraulic_pump=0, 0 , 1.0 propeller_device=0, 0 , 1.0
