[fltsim.0] title=Pan Am A300-600R A sim=a306Rge model= panel= sound= texture= atc_id=N700MS atc_airline=Pan Am atc_flight_number=1123 ui_manufacturer=Airbus ui_type=A300-600R ui_variation=Pan Am visual_damage=1 description=One should hardly be surprised that the world's most prolific manufacturer of commercial aircraft is also the producer of the world's most popular jetliner. The 737 became the best-selling commercial jetliner worldwide when orders for it hit 1,831 in June 1987 (surpassing Boeing's own 727 as the previous champ). However, it wasn't always that way\s in the first few years of production, there were so few orders that Boeing considered canceling the program. They didn't, and the airplane has more than proven itself in over three decades of service. description=Airbus A300-600R by Project Airbus. Modelled by Thomas Ruth, with Textures by Nicholas Wu, Flight Dynamics by Peter Binamira, and Technical Information & Advice by Trevor Slack.\n\n\n\n\n [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 GE CF6-80C2A1.\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 [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=0.002100 inlet_area=96.000000 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=675.425041 [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