[fltsim.0] title=Qantas Posky 767v4 VH-OGF sim=767-300ER-GE-CF6-80C2 model=WV panel= sound= texture= checklists= atc_airline= atc_id=1123 atc_flight_number=940 atc_heavy=1 atc_parking_types=GATE, RAMP, CARGO atc_parking_code= atc_id=VH-OGF ui_manufacturer=Project Opensky ui_type=Boeing 767-300ER ui_variation=Qantas visual_damage=1 description=Project Opensky - Boeing 767-300ER\nVersion 2004.9.8\n\nModel\\VC Designer\n Albert Bouwman \n\nFlight Dynamics\\Sound\\Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Ben Hewitt\n\n2D Panel Designer\n Ed Cox\n\nTechnical Advisors\n Nick Peterson\n Simon Ng\n\nQantas Textures\n David La Rosa\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,115 nautical miles (11,320 km) \n\nTypical city pairs: \n Frankfort-LA [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] performance=Passengers\n3-class conf: 218\n2-class conf: 269 \n\nCargo\nLD-2 containers aft \nTotal lower hold volume: 3,770 cu ft \n\nDimensions\nSpan 156 ft 1 in\nLength 180 ft 3 in\nHeight 52 ft \n\nEngines: GE CF6-80C2\nTO Thrust Rating: 60,800 lb\n\nMax Fuel Cap.: 24,140 gal\nMaxTOW: 409,000 lb\nMax ZFW: 295,000 lb\n\nTypical Cruise Speed \n @ FL350: M.80 atc_type=BOEING atc_model=B763 editable=0 [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 empty_weight = 198443.000 max_gross_weight = 409000.000 max_number_of_stations = 6 // New FS2004 Numbers // Max Structural Payload Per Boeing - 96,557 lbs // Max Structural Payload Opensky - 55,500 lbs // Actual Total PAX - 38,150 lbs station_load.0 =4200.000000, 20.000000, 0.000000, 0.000000, 1st Class - 24 station_load.1 =8050.000000, 40.000000, 0.000000, 0.000000, Bus Class - 46 station_load.2 =25900.000000, 0.000000, 0.000000, 0.000000, Econ Class -148 // Total Opensky Cargo - 17,350 lbs station_load.3 =8175.000000, 45.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd station_load.4 =8175.000000, -50.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft station_load.5 =1000.000000, -70.000000, 0.000000, 0.000000, Lwr Dk Cgo Bulk // Moments of Inertia empty_weight_roll_MOI = 10945212.500 empty_weight_pitch_MOI= 11957602.500 empty_weight_yaw_MOI = 19319851.500 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.201 induced_drag_scalar =1.201 elevator_effectiveness =1.500 aileron_effectiveness =0.550 rudder_effectiveness =0.251 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.751 aileron_trim_effectiveness =0.501 rudder_trim_effectiveness =0.501 [fuel] // Max fuel per Boeing - 767-300 = 16,700 US Gallons / 767-300ER = 24,140 US Gallons Center1 = 0.000, 0.000, 0.000, 7440.000, 3.000 LeftMain = 0.000, -5.000, 0.000, 8350.000, 3.000 RightMain = 0.000, 5.000, 0.000, 8350.000, 3.000 fuel_type = 2.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area= 3050.000 wing_span= 156.083 wing_root_chord= 20.000 wing_dihedral= 6.498 wing_incidence= -1.000 wing_twist= 1.000 oswald_efficiency_factor= 0.653 wing_winglets_flag= 0 wing_sweep= 31.500 wing_pos_apex_lon= 30.000 wing_pos_apex_vert= 0.000 htail_area= 733.000 htail_span= 53.750 htail_pos_lon= -91.667 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 45.000 vtail_area= 325.000 vtail_span= 20.555 vtail_sweep= 35.000 vtail_pos_lon= -87.500 vtail_pos_vert= 5.000 elevator_area= 180.000 aileron_area= 20.000 rudder_area= 56.200 elevator_up_limit= 24.000 elevator_down_limit= 18.000 aileron_up_limit= 24.000 aileron_down_limit= 18.000 rudder_limit= 32.000 elevator_trim_limit= 16.000 spoiler_limit= 45.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 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) // //======================================================================================================================================================= // //FUll Motion, Realistic feel, true footprint contact points //Nose Gear //point.0= 1.000, 76.500, -1.500, -16.500, 2181.102, 0.000, 1.541, 65.000, 1.000, 0.920, 0.650, 9.000, 9.000, 0.000, 280.000, 300.000 //point.1= 1.000, 76.500, 1.500, -16.500, 2181.102, 0.000, 1.541, 65.000, 1.000, 0.920, 0.650, 9.000, 9.000, 0.000, 280.000, 300.000 // //Left Main Gear //point.2= 1.000, -7.000, -15.250, -16.500, 2574.803, 1.000, 1.916, -13.000, 2.500, 0.850, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000 //point.3= 1.000, -7.000, -12.250, -16.500, 2574.803, 1.000, 1.916, -13.000, 2.500, 0.850, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000 //point.4= 1.000, -2.000, -15.250, -17.500, 2574.803, 1.000, 1.916, 0.000, 3.500, 0.892, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000 //point.5= 1.000, -2.000, -12.250, -17.500, 2574.803, 1.000, 1.916, 0.000, 3.500, 0.892, 0.650, 11.900, 11.900, 2.000, 280.000, 300.000 // //Right Main Gear //point.6= 1.000, -7.000, 15.250, -16.500, 2574.803, 2.000, 1.916, -13.000, 2.500, 0.850, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000 //point.7= 1.000, -7.000, 12.250, -16.500, 2574.803, 2.000, 1.916, -13.000, 2.500, 0.850, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000 //point.8= 1.000, -2.000, 15.250, -17.500, 2574.803, 2.000, 1.916, 0.000, 3.500, 0.892, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000 //point.9= 1.000, -2.000, 12.250, -17.500, 2574.803, 2.000, 1.916, 0.000, 3.500, 0.892, 0.650, 13.100, 13.100, 3.000, 280.000, 300.000 // //Scrape Points //point.10= 2.000, -15.000, -78.000, 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 //Left wing //point.11= 2.000, -15.000, 78.000, 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 //Right wing //point.12= 2.000, -87.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Fuse tail //point.13= 2.000, 88.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse nose //point.14= 2.000, -67.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Fuse aft/lower //point.15= 2.000, 72.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse fwd/lower //point.16= 2.000, 6.000, -27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Engine pod/lwrL //point.17= 2.000, 6.000, 27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Engine pod/lwrR //point.18= 2.000, -87.000, 0.000, 37.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Top of vert stab //point.19= 2.000, 72.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Top of fuse/fwd //point.20= 2.000, 60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Top of fuse/fwd //point.21= 2.000, 60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse right/fwd //point.22= 2.000, -60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse right/aft //point.23= 2.000, -60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse left/fwd //point.24= 2.000, -95.000, -30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Horiz stab/left //point.25= 2.000, -95.000, 30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Horiz stab/right //point.26= 2.000, -95.000, 0.000, 45.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Verit stab/aft // //static_pitch= -0.500 //static_cg_height= 14.000 //gear_system_type=0 // //======================================================================================================================================================= // // 3-point, non-realistic feel, non-footprint contact points // //point.0 = 1.000, 76.500, 0.000, -14.750, 2181.102, 0.000, 1.541, 65.000, 0.350, 0.650, 0.850, 9.000, 9.000, 0.000, 280.000, 300.000 //point.1 = 1.000, -4.000, -13.750, -14.750, 2574.803, 1.000, 1.916, -13.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000 //point.2 = 1.000, -4.000, 13.750, -14.750, 2574.803, 2.000, 1.916, -13.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000 //point.3 = 2.000, -15.000, -78.000, 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 //Left wing //point.4 = 2.000, -15.000, 78.000, 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 //Right wing //point.5 = 2.000, -87.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Fuse tail //point.6 = 2.000, 88.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse nose //point.7 = 2.000, -67.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Fuse aft/lower //point.8 = 2.000, 72.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse fwd/lwr //point.9 = 2.000, 6.000, -27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Engine pod/lwrL //point.10= 2.000, 6.000, 27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Engine pod/LwrR //point.11= 2.000, -87.000, 0.000, 37.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //Top vert/stab //point.12= 2.000, 72.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Top fuse/fwd //point.13= 2.000, 60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Top fuse/fwd //point.14= 2.000, 60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse right/fwd //point.15= 2.000, -60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse right/aft //point.16= 2.000, -60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //Fuse left/fwd //point.17= 2.000, -95.000, -30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //Horiz stab/left //point.18= 2.000, -95.000, 30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //Horizstab/right //point.19= 2.000, -95.000, 0.000, 45.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //Vert stab/aft // //static_pitch= -0.500 //static_cg_height= 13.500 //gear_system_type=0 // //======================================================================================================================================================= // // Default with true footprint contact points //Nose Gear point.0= 1.000, 76.500, -1.500, -14.750, 2181.102, 0.000, 1.541, 65.000, 0.350, 0.650, 0.850, 9.000, 9.000, 0.000, 280.000, 300.000 point.1= 1.000, 76.500, 1.500, -14.750, 2181.102, 0.000, 1.541, 65.000, 0.350, 0.650, 0.850, 9.000, 9.000, 0.000, 280.000, 300.000 //Left Main Gear point.2= 1.000, -7.000, -15.250, -14.750, 2574.803, 1.000, 1.916, -13.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000 point.3= 1.000, -7.000, -12.250, -14.750, 2574.803, 1.000, 1.916, -13.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000 point.4= 1.000, -2.000, -15.250, -15.750, 2574.803, 1.000, 1.916, 0.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000 point.5= 1.000, -2.000, -12.250, -15.750, 2574.803, 1.000, 1.916, 0.000, 1.500, 1.200, 0.550, 11.900, 11.900, 2.000, 280.000, 300.000 //Right Main Gear point.6= 1.000, -7.000, 15.250, -14.750, 2574.803, 2.000, 1.916, -13.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000 point.7= 1.000, -7.000, 12.250, -14.750, 2574.803, 2.000, 1.916, -13.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000 point.8= 1.000, -2.000, 15.250, -15.750, 2574.803, 2.000, 1.916, 0.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000 point.9= 1.000, -2.000, 12.250, -15.750, 2574.803, 2.000, 1.916, 0.000, 1.500, 1.200, 0.550, 13.100, 13.100, 3.000, 280.000, 300.000 //Scrape Points point.10= 2.000, -15.000, -78.000, 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 // Left wing point.11= 2.000, -15.000, 78.000, 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 // Right wing point.12= 2.000, -87.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 // Fuse tail point.13= 2.000, 88.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Fuse nose point.14= 2.000, -67.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 // Fuse aft/lower point.15= 2.000, 72.000, -3.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Fuse fwd/lwr point.16= 2.000, 6.000, -27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // Engine pod/lwrL point.17= 2.000, 6.000, 27.000, -9.200, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // Engine pod/LwrR point.18= 2.000, -87.000, 0.000, 37.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // Top of vert/stab point.19= 2.000, 72.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Top of fuse/fwd point.20= 2.000, 60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Top of fuse/fwd point.21= 2.000, 60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Fuse right/fwd point.22= 2.000, -60.000, -9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Fuse right/aft point.23= 2.000, -60.000, 9.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 // Fuse left/fwd point.24= 2.000, -95.000, -30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 // Horiz stab/left point.25= 2.000, -95.000, 30.500, 9.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 // Horiz stab/right point.26= 2.000, -95.000, 0.000, 45.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 // Vert stab/aft static_pitch= -0.500 static_cg_height= 13.500 gear_system_type=0 // //======================================================================================================================================================= // [GeneralEngineData] engine_type= 1 Engine.0= 5.500, -26.667, -5.583 Engine.1= 5.500, 26.667, -5.583 fuel_flow_scalar= 0.7120 min_throttle_limit=-0.319946 [TurbineEngineData] bypass_ratio=4.970 fuel_flow_gain=0.002000 inlet_area=40.68 rated_N2_rpm=29920.000000 static_thrust= 60800.000 afterburner_available= 0 reverser_available= 1.000 [Reference Speeds] flaps_up_stall_speed= 118.000 full_flaps_stall_speed= 94.400 cruise_speed= 452.16 max_indicated_speed=340.000000 max_mach=0.860010 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=81.997949,-2.00,4.00 [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=117.50 //Max N1 = 110.50% for RR RB21, 117.50% for GE CF6, 104.70% for JT9D pitch_takeoff_ga= 0.000 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. 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=0.300000 max_pitch_velocity_lo_alt_breakpoint= 7000.000000 max_pitch_velocity_hi_alt_breakpoint=24000.000000 max_bank=28.000000 max_bank_acceleration=1.200000 max_bank_velocity=1.500000 max_throttle_rate=0.02800 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 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 0, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=Opensky_sparks, 1 touchdown=fx_tchdwn, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 6=taxi, 7=recognition, 8=wing, 9=logo light.1 = 1, 48.500, 0.000, 9.800, Opensky_beacon, // top beacon light.2 = 1, 12.500, 0.000, -8.700, Opensky_beacon, // bottom beacon light.3 = 4, 84.000, 0.000, 3.000, Opensky_Boeing_vclight , // Boeing Orange light.4 = 3, 55.000, 0.000, -4.000, Opensky_nacelle_refl , // front cargo light.5 = 3, -32.000, 0.000, -4.000, Opensky_nacelle_refl , // rear cargo light.6 = 3, 73.000, 0.000, 4.000, Opensky_nacelle_refl , // pax door light.7 = 5, 19.700, 19.000, -4.000, Opensky_nacelle_refl, // nacelle rays from inspection lights light.8 = 5, 19.700, -19.000, -4.000, Opensky_nacelle_refl, // nacelle rays from inspection lights light.9 = 5 18.000, 27.000, -4.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.10= 5, 18.000, -27.000, -4.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.11= 5, 15.500, -45.000, 12.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.12= 5, 15.500, 45.000, 12.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.13= 5, 42.350, 8.350, -0.250, Opensky_nav_yellow , // flap inspection light light.14= 5, 42.350, -8.350, -0.250, Opensky_nav_yellow , // flap inspection light light.15= 5, 28.000, -25.000, 0.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.16= 5, 28.000, 25.000, 0.000, Opensky_wing_light, // wing/LE slat rays from inspection lights light.17= 6, 80.000, 0.000, -8.350, Opensky_wing_light, // gear bay taxi light rays from taxi lights [brakes] toe_brakes_scale=0.43000 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=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] turn_indicator.0=1,0 [TailHook] // For opening cargo door. tailhook_length=1 ;(feet) tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum [folding_wings] // For opening main deck cargo door. wing_fold_system_type = 4 ;0=None fold_rates = 0.05,0.05 ;Percent per second cable_force_adjust = 1.0 [exits] number_of_exits = 2 exit_rate.0 = 0.10 ;Percent per second exit_rate.1 = 0.09 ;Percent per second [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 30.000 system_type= 1 damaging-speed= 200.000 blowout-speed= 250.000 lift_scalar= 0.540 drag_scalar= 0.540 pitch_scalar= 0.500 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 15.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 30.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.540 drag_scalar= 0.540 pitch_scalar= 0.500 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 5.000, 0.000 flaps-position.4= 5.000, 0.000 flaps-position.5= 20.000, 0.000 flaps-position.6= 20.000, 0.000 [jet_engine] thrust_scalar=1.000 [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