[fltsim.0] title=Boeing 777-319ER Air New Zealand sim=Boeing 777-300ER General Electric 90-115B1 model= panel= sound= texture= checklists= atc_airline=New Zealand atc_id=ZK-OKM atc_flight_number=NZ 753 atc_heavy=1 atc_parking_types=GATE,RAMP,CARGO atc_parking_codes=ANZ ui_manufacturer=Boeing ui_type=777-319ER ui_variation=Air New Zealand visual_damage=1 description=Project Opensky Boeing 777-300\nVersion 2-2008.1.0\n\nModel Designers\n Hiroshi Igami\n Yosuke Ube\n\nMaster Textures\n Yosuke Ube\n\nFlight Dynamics Designer\n Brandon D. Henry\n\nFlight Dynamics Assistant\n Philip Foglar\n\nSound Designer\n Emil Serafino\n\nTechnical Resource\n Aaron Seymour\n\nAir New Zealand Livery\n Xudeva Irribarra\n\nTest Pilots\n Project Opensky Members\n\nMaximun Range:\n 7,930 nautical miles (14,685 km)\n\n\nTypical city pairs: \nSan Francisco - Tokyo\nTokyo - Singapore\n Honolulu - Seoul atc_id_color=0x00000000 atc_id_font=Verdana,-11,1,600,0 [weight_and_balance] max_gross_weight = 660000 empty_weight = 347800 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 41600000 empty_weight_roll_MOI = 42000000 empty_weight_yaw_MOI = 67500000 empty_weight_coupled_MOI = 1000 max_number_of_stations = 7 station_load.0 = "4200, 70, 0, 5, 1st Class - 24 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "9450, 40, 0, 5, Business Class - 54 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "28875, -10, 0, 5, Econ Front - 165 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "20125, -55, 0, 5, Econ Rear - 115 pax" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "11250, 50, 0, 0, Fore Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "11250, -50, 0, 0, Aft Cargo " //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "1000, -70, 0, 0, Bulk Cargo" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, 28.5, 0, 12.4, Opensky_beacon light.1 = 1, 4.75, 0, -9, Opensky_beacon light.2 = 3, -127, 0, 4.5, Opensky_nav_yellow light.3 = 8, 32.7, -10.1, 1.3, Opensky_nav_yellow light.4 = 8, 32.7, 10.1, 1.3, Opensky_nav_yellow light.5 = 4, 105, 0, 5.4, Opensky_747_vclight light.6 = 2, -127.9, 0, 8.5, fx_strobeh light.7 = 4, 105, -2.2, 5.328, Opensky_747_vclight light.8 = 4, 105, 2.2, 5.328, Opensky_747_vclight light.9 = 8, 12.5, 23, 0, Opensky_nacelle_refl light.10 = 8, 12.5, -23, 0, Opensky_nacelle_refl light.11 = 8, 25, 30, 0, Opensky_wing_light light.12 = 8, 25, -30, 0, Opensky_wing_light light.13 = 8, 0, 56, 0, Opensky_wing_light light.14 = 8, 0, -56, 0, Opensky_wing_light [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.735 min_throttle_limit = -0.32 engine.0 = 10.0, -32.583, -10.500 engine.1 = 10.0, 32.583, -10.500 [smokesystem] smoke.0 = -15, 22, 32, Opensky_revspray smoke.1 = -15, 22, -32, Opensky_revspray [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = opensky_sparks, 1 touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 3 electric_pump = 1 Center1 = 10, 0, -4, 14220, 10 LeftMain = -5, -35, 0, 6200, 6 LeftAux = -10, -49.705, 0, 9300, 6 RightMain = -5, 35, 0, 6200, 6 RightAux = -10, 49.705, 0, 9300, 6 [contact_points] static_pitch = 0 static_cg_height = 14.5 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 17 //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, 92.500, 0.000, -16.750, 1881.102, 0, 2.0, 70.0, 1.200, 1.800, 1.5, 7.000, 9.000, 0.000, 240.000, 280.000 Point.1= 1, -10.900, -20.291, -18.250, 2574.803, 1, 2.6, 0.0, 1.700, 1.100, 1.5, 10.900, 11.900, 2.000, 240.000, 280.000 Point.2= 1, -10.900, 20.291, -18.250, 2574.803, 2, 2.6, 0.0, 1.700, 1.100, 1.5, 8.100, 13.100, 3.000, 240.000, 280.000 point.3 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.7 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0 point.8 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0 point.9 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.10 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0 point.11 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.12 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.13 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.14 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0 point.15 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0 point.16 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //[contact_points] //static_pitch = 0 //static_cg_height = 16.4 //tailwheel_lock = 0 //gear_system_type = 1 //max_number_of_points = 28 //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, 91.243, -1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280 //point.1 = 1, 91.243, 1.5, -16.5, 1881.102, 0, 1.6, 70, 1, 1.8, 2.4, 7, 9, 0, 240, 280 //point.2 = 1, -14.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.3 = 1, -14.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.4 = 1, -9.800, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.5 = 1, -9.800, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.6 = 1, -5.000, -20.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.7 = 1, -5.000, -15.291, -17.800, 2574.803, 1, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.8 = 1, -14.800, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.9 = 1, -14.800, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.10 = 1, -9.800, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.11 = 1, -9.800, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.12 = 1, -5.000, 20.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 10.9, 11.9, 2, 240, 280 //point.13 = 1, -5.000, 15.291, -17.800, 2574.803, 2, 2, 0, 1.245, 3.0, 2.2, 8.1, 13.1, 3, 240, 280 //point.14 = 2, -44.167, -99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 //point.15 = 2, -44.167, 99.916, 10.000, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 //point.16 = 2, -108, 0, -0.6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //point.17 = 2, 88.417, 0, -7.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //point.18 = 2, 10.000, -32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7.0, 0.0, 0.0 //point.19 = 2, 10.000, 32.583, -8.500, 787.401, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8.0, 0.0, 0.0 //point.20 = 2, 14, -32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 //point.21 = 2, 14, 32.583, -13.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0 //point.22 = 2, 105, 0, -4.5, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //point.23 = 2, 100, 0, 8.9, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //point.24 = 2, -127, 0, 41.3, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //point.25 = 2, -128.5, 35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 5, 9, 0, 0 //point.26 = 2, -128.5, -35, 9, 787.401, 0, 0, 0, 0, 0, 0, 0, 6, 9, 0, 0 //point.27 = 2, -81.5, 0, -6, 787.401, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 [keyboard_response] elevator = 100.000, 200.000 aileron = 100.000, 200.000 rudder = 100.000, 200.000 [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 [airplane_geometry] wing_area = 4605.000 wing_span = 205 wing_root_chord = 50.000 wing_dihedral = 6.218 wing_incidence = 1.000 wing_twist = -0.500 oswald_efficiency_factor = 0.600 wing_winglets_flag = 1 wing_sweep = 35 wing_pos_apex_lon = 30.000 wing_pos_apex_vert = 0.000 htail_area = 1291 htail_span = 70 htail_pos_lon = -96.5 htail_pos_vert = 5 htail_incidence = 0.000 htail_sweep = 40.000 vtail_area = 573.000 vtail_span = 35 vtail_sweep = 45 vtail_pos_lon = -85 vtail_pos_vert = 8.800 elevator_area = 137.000 aileron_area = 68.000 rudder_area = 232.000 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 aileron_to_spoileron_gain = 1.000 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 12.000 min_flaps_for_spoilerons = 0 spoilerons_available = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1.00 parasite_drag_scalar=0.55 induced_drag_scalar=0.88 elevator_effectiveness=1.00 aileron_effectiveness=1.60 rudder_effectiveness=1.00 pitch_stability=1.00 roll_stability=1.00 yaw_stability=1.00 elevator_trim_effectiveness=0.40 aileron_trim_effectiveness=0.50 rudder_trim_effectiveness=0.50 [General] performance=Passengers\n3-class conf: 301 \n2-class conf: N/A \n1-class conf: N/A\n\nCargo\n14 LD-3 containers aft \n600 cubic Ft (17 cubic m)\nTotal lower hold volume: 7,120 cu ft \n\nDimensions\nSpan 212 ft 7 in\nLength 242 ft 4 in\nHeight 61 ft 5 in \n (--max 58 ft 8 in--min)\n\nEngines: General Electric 90-115B1\nTO Thrust Rating: 115,100 lb\n\nMax Fuel Cap.: 47,890 gal\nMaxTOW: 775,000 lb\nZFW: 524,000 lb\n\nMax Range: 7,930 nautical miles (14,685 km)\nTypical Cruise Speed \n @ FL350: M.84 atc_type=BOEING atc_model=B773 editable=0 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI [jet_engine] thrust_scalar=1.000 [TurbineEngineData] bypass_ratio=6.400000 fuel_flow_gain=0.001 inlet_area=65.962 rated_N2_rpm=29920.000 static_thrust=115100.000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=174.000 full_flaps_stall_speed=158.000 cruise_speed=485.00 max_indicated_speed=330.000000 max_mach=0.890020 [Views] eyepoint=103.002, -1.756, 5.20 [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= 110.000 pitch_takeoff_ga=8.00 //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=30.000000 max_bank_acceleration=1.200000 max_bank_velocity=2.000000 max_throttle_rate=0.024 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, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [flaps.0] //Inboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 4.2 // 0.0 .. 1.0 extending-time = 35 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.82 drag_scalar = 0.95 pitch_scalar= 0.60 system_type = 1 //Hydraulic [flaps.1] //Outboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 4.8 // 0.0 .. 1.0 extending-time = 35 // 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 = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.40 drag_scalar = 0.50 pitch_scalar= 0.30 system_type = 1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 4.5 // 0.0 .. 1.0 extending-time = 18 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 5 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 5 // degrees flaps-position.5 = 20 // degrees flaps-position.6 = 20 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.30 drag_scalar = 0.30 pitch_scalar= 0.30 system_type = 1 //Hydraulic [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=0.580 parking_brake=1 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [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 = 0.05,1.00 ;Percent per second [exits] number_of_exits = 4 exit_rate.0 = 0.10 ;Percent per second exit_rate.1 = 0.08 ;Percent per second exit_rate.2 = 0.10 ;Percent per second exit_rate.3 = 0.08 ;Percent per second