[fltsim.0] title=Project Opensky - Boeing 747-400 GOL sim=747-400-GE-CF6-80C2B1 model= panel= sound= texture=1 checklists= atc_airline=GOL atc_flight_number=1695 ui_manufacturer=Boeing ui_type=747-400 ui_variation=Gol Linhas Aéreas visual_damage=1 atc_heavy=1 atc_id=PP-GOG description=Project Opensky Boeing 747-400 repintado nas cores da Gol por Cristiano Magnani [General] performance=Passengers\n3-class conf: 524 \n2-class conf: 416 \n1-class conf: N\/A\n\nCargo\nTotal lower hold volume:\n 5,497 ft3 (155.6 m3) \n\nDimensions\nSpan 211 ft 5 in (213 ft -- fueled)\nLength 231 ft 10 in\nHeight 63 ft 5 in\n\nEngines: GE CF6-80C2B1\nTO Thrust: 54,750 lb x 4\n\nMax Fuel Cap.: 57,065 US Gal.\nMaxTOW: 870,000 lbs\nMLW: 630,000 lbs\nZFW: 545,965 lbs\nOEW: 407,107 lbs\n\nMax Range: 7305 mi \nTypical Cruise Speed \n @ FL350: M.85 atc_type=BOEING atc_model=B744 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 max_number_of_stations=50 //station_load.0=9720,-100.0, 0.0, -11.0 //Aft Bulk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //station_load.1=57500, 80.0, 0.0, 0.0 //LD aft - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //station_load.2=61000, -80.0, 0.0, 0.0 //LD fwd - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //station_load.3=118307, 0.0, 0.0, 0.0 //Main Dk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //station_load.4=2640, 47.0, 0.0, 20.005434 //Upper Dk - Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight=545965.000 empty_weight_roll_MOI=9857983.000 empty_weight_pitch_MOI=20732658.000 empty_weight_yaw_MOI=31205473.000 empty_weight_coupled_MOI=0.000 max_gross_weight=928300.489 CG_forward_limit=0.000 CG_aft_limit=1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [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 electric_pump=1 [airplane_geometry] wing_area=5650.000 wing_span=211.000 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=1 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=24.000 elevator_down_limit=18.000 aileron_up_limit=20.000 aileron_down_limit=20.000 rudder_limit=30.000 elevator_trim_limit=9.167 spoiler_limit=45.000 spoilerons_available=0 aileron_to_spoileron_gain=3.000 min_ailerons_for_spoilerons=11.459 min_flaps_for_spoilerons=0.000 [Reference Speeds] flaps_up_stall_speed=150.0 //Knots True (KTAS) full_flaps_stall_speed=126.0 //Knots True (KTAS) cruise_speed=495.0 //Knots True (KTAS) max_indicated_speed=350.000000 max_mach=0.900000 [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=0.28 drag_scalar=0.40 pitch_scalar=0.40 system_type=1 //Hydraulic [flaps.1] type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 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=0.28 drag_scalar=0.40 pitch_scalar=0.40 system_type=1 //Hydraulic [flaps.2] 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=0.28 drag_scalar=0.40 pitch_scalar=0.40 system_type=1 //Hydraulic [flaps.3] type=2 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=12 // seconds flaps-position.0=0 // degrees flaps-position.1=20 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.28 drag_scalar=0.40 pitch_scalar=0.40 system_type=1 //Hydraulic [flaps.4] type=2 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=12 // seconds flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=20.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=0.28 drag_scalar=0.40 pitch_scalar=0.40 system_type=1 //Hydraulic [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 [GeneralEngineData] engine_type=1 Engine.0=-14.917, -69.500, 0.000 Engine.1=14.917, -39.167, -7.000 Engine.2=14.917, 39.167, -7.000 Engine.3=-14.917, 69.500, 0.000 fuel_flow_scalar=0.9676 min_throttle_limit=-0.319946 [TurbineEngineData] bypass_ratio=4.800000 fuel_flow_gain=0.001 inlet_area=48.150 rated_N2_rpm=29992.000 static_thrust=54750.000 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.0 [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=8.000000 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=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=0.000000 [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, 2181.102, 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, 2574.803, 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, 2574.803, 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, -49.000, -102.900, 7.000, 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, -49.000, 102.900, 7.000, 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, -92.667, 0.000, -2.000, 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.6=2.000, 88.167, 0.000, -5.750, 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,-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 point.8=2.000, -14.917, -69.500, -7.000, 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.9=2.000, 14.917, -39.167, -11.000, 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.10=2.000, 14.917, 39.167, -11.000, 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.11=2.000, -14.917, 69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch=-1.000 static_cg_height=13.125 // Nose gear //point.0=1.000, 67.333, -1.500, -15.333, 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, -15.333, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -17.133, 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, -49.000, -102.900, 7.000, 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, -49.000, 102.900, 7.000, 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 -92.667, 0.000, -2.000, 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.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, -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 //point.23=2.000, -14.917, -69.500, -7.000, 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.24=2.000, 14.917, -39.167, -11.000, 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.25=2.000, 14.917, 39.167, -11.000, 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.26=2.000, -14.917, 69.500, -7.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 // //static_pitch=-1.000 //static_cg_height=13.625 gear_system_type=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 [Views] eyepoint=83.000, -2.000, 14.800 // Longitude, Latitude and Vertical position from Reference Point, (FEET) [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=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 [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 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=100, 200 aileron=100, 200 rudder=100, 200 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=Opensky_sparks, 1 touchdown=fx_tchdwn, 1 [SMOKESYSTEM] //Aileron tip vortecies smoke.0=0, -30.167, -86.167, Opensky_vortex smoke.1=0, -30.167, 86.167, Opensky_vortex //Wing condensation smoke.2=0, -08.917, -39.167, Opensky_conden smoke.3=0, -08.917, 39.167, Opensky_conden [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=1, 65.200, 0.600, 19.100, Opensky_beacon , light.1=1, 13.500, 0.000, -7.080, Opensky_beacon , light.2=2, -49.000, -102.900, 13.150, fx_strobeh , light.3=2, -49.000, 102.900, 13.150, fx_strobeh , light.4=3, -122.700, -0.250, 12.300, Opensky_nav_yellow , light.5=3, -122.700, 0.250, 12.300, Opensky_nav_yellow , light.6=2, -121.900, 0.000, 11.450, fx_strobeh , light.7=3, 84.850, 0.000, 14.850, fx_vclighth , light.8=3, -111.500, -4.500, 43.750, Opensky_wing_light , light.9=3, -111.500, 4.500, 43.750, Opensky_wing_light , light.10=5, 18.700, -29.200, -2.000, Opensky_nacelle_refl , light.11=5, 18.700, 29.200, -2.000, Opensky_nacelle_refl , light.12=5, 51.500, -11.700, 0.000, Opensky_nacelle_refl , light.13=5, 51.500, 11.700, 0.000, Opensky_nacelle_refl , light.14=5, 57.500, -13.700, 1.900, Opensky_nacelle_refl , light.15=5, 57.500, 13.700, 1.900, Opensky_nacelle_refl , light.16=5, 83.333, 0.000, -2.000, Opensky_nacelle_refl , light.17=3, 72.300, -6.500, 6.000, Opensky_nacelle_refl , light.18=3, 45.610, -4.500, 6.000, Opensky_nacelle_refl , light.19=3, -47.510, 0.000, -3.000, Opensky_wing_light , [brakes] toe_brakes_scale=0.915555 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
