[fltsim.0] title=Airbus A300-600 BERUGA sim=pac300600stge model= panel= sound= texture= checklists= description=AIRBUS A300-600ST\n\nThe A300-600 is optimised for maximum profitability in the demanding mid-size regional market. With the capability to operate profitably on extended range routes, it incorporates many technological features not found on competing airliners. These improve reliability and reduce operating costs. The A300-600 layout and has a range of 4,000 nm\/7,700 km.\n\n\n\n\n\n\n ui_manufacturer= ui_type=AIRBUS A300-600 ui_variation= atc_heavy=0 atc_id= atc_airline=AIRBUS atc_flight_number=BLG01 [General] performance=The overall length: 56.20 m \nSpan: 44.84 m \nAll high 17.23 m \nInstallation capacity main deck : 1,400 m3 (49,440 ft3) \nUnderfloor bulk :17.3 m3 (611 ft3) \nInstallation weight: 47,000 kg (103,590 lb.) \nTakeoff weight :155,000 kg (341,713 lb.) \nsecond series distance: 1,660-4,632 km \nCruising speed :0.7 Mach \nMost ultrahigh altitude: 10,670 m (35,000 ft.)\n\nMake by AKIRA TAKAHSHI atc_type= atc_model=A330 [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=0.000000,0.000000,0.000000,0.000000 empty_weight= 275000.000 empty_weight_roll_MOI= 22080000.000 empty_weight_pitch_MOI= 19280000.000 empty_weight_yaw_MOI= 14500000.000 empty_weight_coupled_MOI= 650000.000 max_gross_weight= 395633.497 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, -4.000, 6275.000, 3.000 LeftMain= -7.000, -30.000, 0.000, 5865.000, 3.000 RightMain= -7.000, 30.000, 0.000, 5865.000, 3.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 2800.000 wing_span= 147.000 wing_root_chord= 19.083 wing_dihedral= 3.598 wing_incidence= 1.000 wing_twist= -0.994 oswald_efficiency_factor= 0.932 wing_winglets_flag= 65535 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=-1 aileron_to_spoileron_gain=0.140000 min_ailerons_for_spoilerons=9.969466 min_flaps_for_spoilerons=0.000000 [contact_points] point.0= 1.000, 52.750, 0.000, -13.583, 1574.803, 0.000, 3.243, 67.980, 0.560, 2.500, 0.474, 12.000, 12.000, 0.000, 0.000, 0.000 point.1= 1.000, -9.750, -16.250, -14.583, 1574.803, 1.000, 3.243, 0.000, 0.573, 2.500, 0.468, 14.000, 14.000, 2.000, 0.000, 0.000 point.2= 1.000, -9.750, 16.250, -14.583, 1574.803, 2.000, 3.243, 0.000, 0.573, 2.500, 0.468, 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= 15.448 [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= 0.003 inlet_area= 105.600 rated_N2_rpm= 30150.000 static_thrust= 59000.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 145.000 full_flaps_stall_speed= 116.000 cruise_speed= 318.787 [keyboard_response] elevator=136.000000,222.000000 aileron=173.000000,254.000000 rudder=300.000000,300.000000 [Views] eyepoint=65.116982,-2.332472,0.102526 [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 [jet_engine] thrust_scalar = 1.35 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 20.000 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