[fltsim.0] title=Opensky 747 GE Engine test sim=747-200PW model= panel= sound= texture=GE checklists= atc_airline=Ge atc_flight_number=204 ui_manufacturer=Boeing Project Opensky ui_type=747-200 ui_variation=GE visual_damage=1 atc_heavy=1 atc_id=N747GE description=Project Opensky \nBoeing 747-200\nVersion 2004.1.1.0\n\nEngine Type PW JT9D-7R4G2\n\n747-200 Commercial Version \n\nModel Designer\n Yosuke Ube\n Vincent Cho\n\nFlight Dynamics Designer\n Nick Peterson, based on original by Warren Daniel\n\nTechnical Resource\n Simon Ng\n Shigeo Kitaguchi\n\nTest Pilots\n Paint by Hugo Espinosa "focus@newyork.com" [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: PW JT9D-7R4G2\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 52,410 US Gal.\nMaxTOW: 833,000 lbs\nMLW: 630,000 lbs\nZFW: 460,340 lbs\nOEW: 388,010 lbs\n\nMax Range: 5,650 nm\nTypical Cruise Speed \n @ FL350: M.84 atc_type=BOEING AIRCRAFT atc_model=B742 editable=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 [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 [WEIGHT_AND_BALANCE] reference_datum_position= 88.000, 0.000, 0.000 empty_weight_CG_position= -105.000, 0.000, 0.000 empty_weight=386850 empty_weight_roll_MOI= 18155743.000 empty_weight_pitch_MOI= 17600873.000 empty_weight_yaw_MOI= 19151035.000 empty_weight_coupled_MOI= 0.000 max_gross_weight=833000 max_number_of_stations= 6 station_load.0 = "3060.0, -19.0, 0.0, 2.0, 1stClass 17Pax" station_load.1 = "2800.0, -48.00, 0.0,14.0, Upp Deck 42Pax" station_load.2 = "7020.0, -83.0, 0.0, 2.0, Bus Class 39Pax" station_load.3 = "50040.0, -118.0, 0.0, 2.0, Coach 278Pax" station_load.4 = "18000.0, -63.0, 0.0,-2.0, Forward Cargo" station_load.5 = "16000.0, -120, 0.0,-2.0, Aft Cargo" [fuel] Center1 = -88.0, 0.0, -4.0, 19431.0, 3.0 LeftMain =-102.0, -35.0, -4.0, 16660.0, 3.0 LeftAux =-109.5, -52.0, -3.0, 500.0, 3.0 RightMain =-102.0, 35.0, -4.0, 16660.0, 3.0 RightAux =-109.5, 52.0, -3.0, 500.0, 3.0 fuel_type =2.000000 electric_pump=1 number_of_tank_selectors=1 [airplane_geometry] wing_area= 5500.000 wing_span= 196.000 wing_root_chord= 53.000 wing_dihedral= 3.998 wing_incidence= 3.500 wing_twist= -0.194 oswald_efficiency_factor= 0.730 wing_winglets_flag= 0 wing_sweep= 37.500 wing_pos_apex_lon= -78.000 wing_pos_apex_vert= 0.000 htail_area= 1470.000 htail_span= 72.750 htail_pos_lon= -204.167 htail_pos_vert= 7.000 htail_incidence= 0.000 htail_sweep= 37.500 vtail_area= 1060.000 vtail_span= 37.121 vtail_sweep= 45.000 vtail_pos_lon= -204.500 vtail_pos_vert= 6.083 elevator_area= 326.800 aileron_area= 225.200 rudder_area= 229.900 elevator_up_limit= 20.751 elevator_down_limit= 15.313 aileron_up_limit= 31.513 aileron_down_limit= 31.513 rudder_limit= 17.189 elevator_trim_limit= 19.167 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] point.0= 1.000, -21.333, 0.00, -14.853, 1181.102, 0.000, 2.000, 70.000, 1.129, 1.100, 0.98, 9.000, 11.000,0.000, 240.000, 280.000 point.1= 1.000, -99.583, -16.000, -15.403, 1574.803, 1.000, 2.000, 0.000, 1.62, 1.15, 0.741, 12.900, 14.900, 2.000, 240.000, 280.000 point.2= 1.000, -99.583, 16.000, -15.403, 1574.803, 2.000, 2.000, 0.000, 1.62, 1.15, 0.741, 13.100, 15.400, 3.000, 240.000, 280.000 point.3= 1.000, -109.583, -6.000, -15.403, 1574.803, 1.000, 2.000, 13.000, 1.62, 1.15, 0.741, 13.400, 14.900, 2.000, 240.000, 280.000 point.4= 1.000, -109.583, 6.000, -15.403, 1574.803,2.000, 2.000, 13.000,1.62, 1.15, 0.741, 12.500, 13.500, 3.000, 240.000, 280.000 point.5= 2.000, -102.167, -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.6= 2.000, -102.167, 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.7= 2.000, -220.667, 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.8= 2.000, 0.0, 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.9= 2.000, -102.167, -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.10= 2.000, -220.667, 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= -.300 static_cg_height= 13.625 gear_system_type=0 [GeneralEngineData] engine_type=1 Engine.0=-109.916667,-69.500000,0.000000 Engine.1=-86.916667,-39.166667,-7.000000 Engine.2=-86.916667,39.166667,-7.000000 Engine.3=-109.916667,69.500000,0.000000 fuel_flow_scalar=1.04 min_throttle_limit=-0.399902 [TurbineEngineData] bypass_ratio=4.970000 fuel_flow_gain=0.002000 inlet_area=37.558941 rated_N2_rpm=29920.000000 static_thrust=54750.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed= 150.000 full_flaps_stall_speed= 126.000 cruise_speed= 524.337 max_indicated_speed=350.000000 max_mach=0.900000 [keyboard_response] elevator= 100.000, 200.000 aileron= 100.000, 200.000 rudder= 150.000, 250.000 [Views] eyepoint=-9.000, -2.000, 14.800 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=105.000000 pitch_takeoff_ga=14.000000 use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank = 1 // 0 = Def default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [flaps.0] type = 1 span-outboard = 0.4 extending-time = 25 flaps-position.0 = 0 flaps-position.1 = 5 flaps-position.2 = 10 flaps-position.3 = 15 flaps-position.4 = 20 flaps-position.5 = 25 flaps-position.6 = 30 damaging-speed = 200 blowout-speed = 250 lift_scalar = 1.00 drag_scalar = .67 pitch_scalar= 0.3 system_type = 1 [flaps.1] type = 1 span-outboard = 0.4 extending-time = 25 flaps-position.0 = 0 flaps-position.1 = 5 flaps-position.2 = 10 flaps-position.3 = 15 flaps-position.4 = 20 flaps-position.5 = 25 flaps-position.6 = 30 damaging-speed = 200 blowout-speed = 250 lift_scalar = 1.00 drag_scalar = .67 pitch_scalar= 0.3 system_type = 1 [flaps.2] type = 2 span-outboard = 0.8 extending-time = 12 flaps-position.0 = 0 flaps-position.1 = 20.0 damaging-speed = 250 blowout-speed = 300 lift_scalar = 0.67 drag_scalar = .4 pitch_scalar= 0.1 system_type = 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 [folding_wings] // For opening main deck cargo door. wing_fold_system_type = 4 ;0=None fold_rates = 0.070, 0.070 ;Percent per second cable_force_adjust = 1.0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 exit_rate.1 = 0.4 [TailHook] // For opening cargo door. tailhook_length=1 ;(feet) tailhook_position = 0.0, 0.0, 0.0 fold_rates = .070, .07 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, -22.95, 0.600, 19.100, Opensky_beacon , light.1 = 1, -74.500, 0.000, -7.080, Opensky_beacon , light.2 = 2, -130.00, -95.000, 8.80, fx_strobeh , light.3 = 2, -130.00, 95.000, 8.80, fx_strobeh , light.4 = 3, -210.700, -0.250, 12.300, Opensky_nav_yellow , light.5 = 3, -210.700, 0.250, 12.300, Opensky_nav_yellow , light.6 = 2, -210.900, 0.000, 11.450, fx_strobeh , light.7 = 3, -4.850, 0.000, 14.850, fx_vclighth , light.8 = 3, -199.500, -4.500, 43.750, Opensky_wing_light , light.9 = 3, -199.500, 4.500, 43.750, Opensky_wing_light , light.10= 5, -70.700, -29.200, 0.000, Opensky_nacelle_refl , light.11= 5, -70.700, 29.200, 0.000, Opensky_nacelle_refl , light.12= 5, -37.500, -11.700, 2.000, Opensky_nacelle_refl , light.13= 5, -37.500, 11.700, 2.000, Opensky_nacelle_refl , light.14= 5, -31.500, -13.700, 3.900, Opensky_nacelle_refl , light.15= 5, -31.500, 13.700, 3.900, Opensky_nacelle_refl , light.16= 5, -5.333, 0.000, -2.000, Opensky_nacelle_refl , light.17= 3, -9.300, -6.500, 6.000, Opensky_nacelle_refl , light.18= 3, -43.610, -4.500, 6.000, Opensky_nacelle_refl , light.19= 3, -135.510, 0.000, -3.000, Opensky_wing_light , [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 [Radios] // Radio Type = available, 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 [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 [brakes] toe_brakes_scale=.90555 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0