[fltsim.0] title=Varig B767-27GER PR-VAC circa 2007 sim=767-200ER-GE-CF6-80A model= panel= sound= texture= checklists= atc_airline=Transbrasil atc_id=PR-VAC atc_flight_number=621 atc_heavy=1 atc_parking_types=GATE atc_parking_code=VRG ui_manufacturer=project Opensky ui_type=767-200 ui_variation=Varig B767-27GER PR-VAC circa 2007 visual_damage=1 description=Project Opensky Boeing - 767-200ER\nVersion 2004.9.4\n\nModel\\VC Designer\n Albert Bouwman \n\nFlight Dynamics\\Sound\\Effects Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Ben Hewitt, Dickson Chan\n\\Livery: Ricardo Lin\n\n2D Panel Designer\n Ed Cox\n\nTechnical Advisors\n Nick Peterson\n Simon Ng\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range: 6,115 nautical miles (11,320 km) \n\nModel Information: PT-TAH was delivered on 23\/02\/1995 and returned to lessor on 10\/11\/1999. [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: 174\n\nCargo\nTotal lower hold volume: 22 LD2 \n\nDimensions\nSpan 156 ft 1 in\nLength 159 ft 2 in\nHeight 52 ft \n\nEngines: GE CF6-80A2\nTO Thrust Rating: 50,000 lb\n\nMax Fuel Cap.: 16,700 gal\nMaxTOW: 345,000 lb\nTypical ZFW: 209,000 lb\n\nTypical Cruise Speed \n @ FL350: M.78 atc_type=BOEING atc_model=B767 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 = 181350.000 max_gross_weight = 352200.000 max_number_of_stations = 6 // New FS2004 Numbers // Max Structural Payload Per Boeing - 78,500 lbs // Max Structural Payload Opensky - 44,500 lbs // Actual Total PAX - 38,150 lbs station_load.0 =2550.000000, 45.000000, 0.000000, 0.000000, 1st Class - 15 station_load.1 =6800.000000, 20.000000, 0.000000, 0.000000, Bus Class - 40 station_load.2 =20230.000000, 0.000000, 0.000000, 0.000000, Econ Class -119 // Total Opensky Cargo - 17,350 lbs station_load.3 =6525.000000, 35.000000, 0.000000, 0.000000, Lwr Dk Cgo Fwd station_load.4 =6525.000000, -22.000000, 0.000000, 0.000000, Lwr Dk Cgo Aft station_load.5 =200.000000, -44.000000, 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 - 767-200 = 16,700 US Gallons / 767-200ER = 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= -70.667 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= -66.500 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, 66.500, -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, 66.500, 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, -66.000, 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, 78.000, 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, -46.000, -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, 62.000, -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, -66.000, 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, 62.000, 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, 50.000, -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, -74.000, -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, -74.000, 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, -74.000, 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= 14.000 //gear_system_type=0 // //======================================================================================================================================================= // // 3-point, non-realistic feel, non-footprint contact points // //point.0 = 1.000, 66.500, 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, -66.000, 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, 78.000, 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, -46.000, -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, 62.000, -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, -66.000, 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.12= 2.000, 62.000, 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.13= 2.000, 50.000, -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.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, -74.000, -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, -74.000, 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.19= 2.000, -74.000, 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, 66.500, -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, 66.500, 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 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 point.12= 2.000, -66.000, 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 point.13= 2.000, 78.000, 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 point.14= 2.000, -46.000, -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 point.15= 2.000, 62.000, -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 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 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 point.18= 2.000, -66.000, 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 point.19= 2.000, 62.000, 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 point.20= 2.000, 50.000, -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 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 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 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 point.24= 2.000, -74.000, -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 point.25= 2.000, -74.000, 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, -74.000, 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= 0.712 min_throttle_limit=-0.319946 [TurbineEngineData] bypass_ratio=4.970 fuel_flow_gain= 0.002 inlet_area= 40.680 rated_N2_rpm= 29920.000 static_thrust= 50000.000 afterburner_available= 0 reverser_available= 1.000 [Reference Speeds] flaps_up_stall_speed= 118.000 full_flaps_stall_speed= 94.400 cruise_speed= 452.160 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=71.997949,-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, 42.000, 0.000, 9.800, Opensky_beacon, // top beacon light.2 = 1, 12.500, 0.000, -8.700, Opensky_beacon, // bottom beacon light.3 = 4, 74.000, 0.000, 3.000, Opensky_Boeing_vclight , // Boeing Orange light.4 = 3, 30.000, 0.000, -4.000, Opensky_nacelle_refl , // front cargo light.5 = 3, -20.000, 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, 32.350, 8.350, -0.250, Opensky_nav_yellow , // flap inspection light light.14= 5, 32.350, -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, 72.000, 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 [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 [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