[fltsim.0] title=Lufthansa sim=a306Rge model= panel= sound= texture= checklists= ui_manufacturer=Airbus ui_type=A300-600R ui_variation=Lufthansa description=Lufthansa currently operates 3 of the long ranger -605R aircraft, with one more on order. It is configured to 270 seats. Lufthansa also operates 10 A300-603 aircraft. Lufthansa Airbus A300-600R D-AIAX FÜRTH.\nModel by Steffen Gedamke,\nFlight Dynamics by Steffen Gedamke,\nTextures by Steffen Gedamke\n\nw23jk@lycos.de atc_heavy=0 atc_id=D-AIAX atc_airline=LUFTHANSA atc_flight_number=LH603 [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= 196025.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 station_load.0= 420.000, 41.000, 0.000, 0.000 station_load.1= 4000.000, 19.000, 0.000, 0.000 station_load.2= 8000.000, 28.000, 0.000, 0.000 station_load.3= 18000.000, 3.000, 0.000, 0.000 station_load.4= 8000.000, -40.000, 0.000, 0.000 station_load.5= 6340.000, 25.000, 0.000, 0.000 station_load.6= 9220.000, 30.000, 0.000, 0.000 station_load.7= 14480.000, 18.000, 0.000, 0.000 station_load.8= 13480.000, -83.000, 0.000, 0.000 //total load=81,940lbs + ZFW 196,025= 277,965lbs or 126,348kgs empty_weight_roll_MOI= 9080000.000 empty_weight_pitch_MOI= 13280000.000 empty_weight_yaw_MOI= 9500000.000 empty_weight_coupled_MOI= 650000.000 max_gross_weight= 437277.595 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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 atc_type=AIRBUS atc_model=A306 [fuel] Center1= 0.000, 0.000, -4.000, 5232.000, 3.000 LeftMain= -7.000, -30.000, 0.000, 9273.000, 3.000 RightMain= -7.000, 30.000, 0.000, 9273.000, 3.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 2700.000 wing_span= 147.000 wing_root_chord= 19.083 wing_dihedral= 3.598 wing_incidence= 0.758 wing_twist= 2.296 oswald_efficiency_factor= 0.869 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 748.000 htail_span= 53.333 htail_pos_lon= -84.000 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 487.000 vtail_span= 25.161 vtail_sweep= 0.000 vtail_pos_lon= -81.667 vtail_pos_vert= 28.250 elevator_area= 69.000 aileron_area= 44.240 rudder_area= 69.700 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.140 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 52.750, 0.000, -13.833, 1574.803, 0.000, 3.531, 67.980, 0.571, 2.500, 0.912, 13.000, 13.000, 0.000, 0.000, 0.000 point.1= 1.000, -9.750, -16.250, -15.333, 1574.803, 1.000, 3.531, 0.000, 2.043, 2.500, 1.273, 14.600, 14.600, 2.000, 0.000, 0.000 point.2= 1.000, -9.750, 16.250, -15.333, 1574.803, 2.000, 3.531, 0.000, 2.043, 2.500, 1.273, 15.000, 15.000, 3.000, 0.000, 0.000 point.3= 2.000, -28.083, -74.083, 2.583, 1574.803, 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, -28.083, 74.083, 2.583, 1574.803, 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, -79.667, 0.000, 1.333, 1574.803, 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, 56.417, 0.000, 1.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.912 static_cg_height= 13.546 [GeneralEngineData] engine_type= 1 Engine.0= 8.583, -11.500, -3.167 Engine.1= 8.583, 11.500, -3.167 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 96.000 rated_N2_rpm= 30150.000 static_thrust= 49000.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 145.000 full_flaps_stall_speed= 116.000 cruise_speed= 675.425 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 27.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 9.998, 0.000 flaps-position.2= 19.996, 0.000 flaps-position.3= 29.994, 0.000 flaps-position.4= 39.992, 0.000