[fltsim.0] title=Airbus A300-600R QANTAS Airways sim=a306Rpw model= panel= sound= texture= checklists= atc_id=VH-tAA atc_airline=QANTAS atc_flight_number=2947 ui_manufacturer=Qantas ui_type=A300-600 ui_variation=Qantas Airways visual_damage=1 description=Airbus A300-600R by Project Airbus\nModelled by Thomas Ruth, with Textures by Nicholas Wu, Flight Dynamics by Peter Binamira, and Technical Information & Advice by Trevor Slack. atc_heavy=1 [forcefeedback] stick_shaker_magnitude=3000 stick_shaker_direction=0 stick_shaker_period=111111 gear_bump_nose_magnitude=3000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2700 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=2700 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1600 ground_bumps_angle1=8900 ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=400 ground_bumps_angle2=9100 ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [jet_engine] thrust_scalar=1.131 [flight_tuning] pitch_stability=0.751 roll_stability=0.920 yaw_stability=0.820 elevator_effectiveness=1.401 aileron_effectiveness=2.101 rudder_effectiveness=2.701 [WEIGHT_AND_BALANCE] empty_weight = 196025 // (pounds) reference_datum_position = 0.0, 0, 0 empty_weight_CG_position = 0.0, 0, 0 station_load.0 = 0420, 41.00, 0.0, 0.0 //Weight Crew (lbs) LEAVE station_load.1 = 4000, 19.00, 0.0, 0.0 //Weight Galleys(lbs) LEAVE station_load.2 = 8000, 28.00, 0.0, 0.0 //Weight Baggage 1 (lbs) Baggage A | station_load.3 = 18000, 3.00, 0.0, 0.0 //Weight Baggage 2 (lbs) CARGO | station_load.4 = 8000, -40.00, 0.0, 0.0 //Weight Baggage 3 (lbs) Baggage B | station_load.5 = 6340, 25.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs) First ---- |--140 lb PER PASSANGER station_load.6 = 9220, 30.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs) Mabuhay Class| station_load.7 = 14480, 18.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs) Economy A | station_load.8 = 13480, -83.00, 0.0, 0.0 //Weight Psgr Sect OD (lbs) Economy B | //total load= 81,940lbs + ZFW 196,025= 277,965lbs or 126,348kgs empty_weight_roll_MOI=9080000.000000 empty_weight_pitch_MOI=13280000.000000 empty_weight_yaw_MOI=9500000.000000 empty_weight_coupled_MOI=650000.000000 [electrical] max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 40.0 avionics_bus = 0, 0, 1 avionics = 1, 0, 1 starter1 = 0, 0, 1 starter2 = 0, 0, 1 fuel_transfer_pump = 0, 0, 1 flap_motor = 0, 0, 1 gear_motor = 0, 0, 1 autopilot = 0, 0, 1 pitot_heat = 0, 0, 1 additional_system = 0, 0, 1 marker_beacon = 1, 0, 1 gear_warning = 0, 0, 1 fuel_pump = 0, 0, 1 light_nav = 0, 0, 1 light_beacon = 0, 1, 1 light_landing = 0, 0, 1 light_taxi = 0, 0, 1 light_strobe = 0, 1, 1 light_panel = 0, 0, 1 auto_brake = 0, 0, 1 standby_vacuum = 0, 0, 1 hydraulic_pump = 0, 0, 1 light_recognition = 0, 0, 1 light_wing = 0, 0, 1 light_logo = 0, 0, 1 //aircraft.cfg file by Peter Binamira. Must be used with the PA A300-600R aircrafts. 09/30/01 //PA A300-600R .air files won't be optimized without this aircraft.cfg file. [General] performance=Max cruising speed: 897km\/h \nRange at typical airline operating weight: 7540km (4070nm) with PW4000.\nDimensions: Wing span 44.84m (147ft 1in), length 54.08m (177ft 5in), height 16.62m (54ft 6.5in).\n [fuel] Center1=0.000000,0.000000,-4.000000,5232.000000,3.000000 LeftMain=-7.000000,-30.000000,0.000000,9273.000000,3.000000 RightMain=-7.000000,30.000000,0.000000,9273.000000,3.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=2700.000000 wing_span=147.000000 wing_root_chord=19.083333 wing_dihedral=3.598022 wing_incidence=0.758057 wing_twist=2.296143 oswald_efficiency_factor=0.868836 wing_winglets_flag=65281 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=748.000000 htail_span=53.333333 htail_pos_lon=-84.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=487.000000 vtail_span=25.161478 vtail_sweep=0.000000 vtail_pos_lon=-81.666667 vtail_pos_vert=28.250000 elevator_area=69.000000 aileron_area=44.240000 rudder_area=69.700000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.140000 min_ailerons_for_spoilerons=9.969466 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,52.750000,0.000000,-13.833333,1574.803150,0.000000,3.531387,67.980000,0.571490,2.500000,0.912014,13.000000,13.000000,0.000000,0.000000,0.000000 point.1=1.000000,-9.750000,-16.250000,-15.333333,1574.803150,1.000000,3.531387,0.000000,2.043271,2.500000,1.272533,14.600000,14.600000,2.000000,0.000000,0.000000 point.2=1.000000,-9.750000,16.250000,-15.333333,1574.803150,2.000000,3.531387,0.000000,2.043271,2.500000,1.272533,15.000000,15.000000,3.000000,0.000000,0.000000 point.3=2.000000,-28.083333,-74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-28.083333,74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-79.666667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,56.416667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=-0.911865 static_cg_height=13.545886 [SMOKESYSTEM] smoke.0=-2.50,0.25,-16.1, fx_smoke_rx smoke.1=-2.50,0.25,16.1, fx_smoke_rx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [Flaps.0] type=1 span-outboard=0.500000 extending-time=27.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=9.998114,0.000000 flaps-position.2=19.996227,0.000000 flaps-position.3=29.994341,0.000000 flaps-position.4=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=8.583333,-11.500000,-3.166667 Engine.1=8.583333,11.500000,-3.166667 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.001980 inlet_area=97.000000 rated_N2_rpm=30150.000000 static_thrust=49000.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=145.000000 full_flaps_stall_speed=116.000000 cruise_speed=679.340581 [keyboard_response] elevator=116.000000,180.000000 aileron=113.000000,174.000000 rudder=300.000000,300.000000 [Views] eyepoint=65.898745,-2.153051,7.215285 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0