[fltsim.0] title=Concorde Qantas Airways sim=Concorde model= panel= sound= texture= kb_checklists=Concorde_check kb_reference=Concorde_ref atc_id=G-BOAC atc_id_enable=1 atc_airline=Qantas atc_flight_number=1123 ui_manufacturer=Aerospatiale ui_type=Concorde ui_variation=Qantas Airways visual_damage=1 description=See ref notes for detatails. [General] performance=Max speed 2,5 Mach\nCruise speed 2 Mach\nMax range 3371 mn \nCealing 60000 feet [WEIGHT_AND_BALANCE] empty_weight=172930.0 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-50.333, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum station_load.0=1760, 1.00, 0.0, 0.0 //Weight Crew (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=3342, -29.00, 0.0, 0.0 //Weight Galleys(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=300, 8.00, 0.0, 0.0 //Weight Baggage 1 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=500, -4.00, 0.0, 0.0 //Weight Baggage 2 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=2562, -82.00, 0.0, 0.0 //Weight Baggage 3 (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=3040, 18.00, 0.0, 0.0 //Weight Psgr Sect OA (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=3040, 2.00, 0.0, 0.0 //Weight Psgr Sect OB (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=4370, -28.00, 0.0, 0.0 //Weight Psgr Sect OC (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8=6080, -53.00, 0.0, 0.0 //Weight Psgr Sect OD (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_roll_MOI=695703.000000 empty_weight_pitch_MOI=9295118.000000 empty_weight_yaw_MOI=4906663.000000 empty_weight_coupled_MOI=0.000000 [ground_reaction] main_gear_static_compression=1.5 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=1.5 // (feet), The distance the center gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.95 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.95 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) fuel_transfer_pump=0, 10, 17.0 [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 [contact_points] point.0=1.000000,5.666667,0.000000,-15.500000,1181.102362,0.000000,3.336104,34.080000,1.500000,2.500000,0.950000,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-54.000000,-13.000000,-15.000000,1574.803150,1.000000,3.336104,0.000000,1.500000,2.500000,0.950000,7.900000,7.900000,2.000000,0.000000,0.000000 point.2=1.000000,-54.000000,13.000000,-15.000000,1574.803150,2.000000,3.336104,0.000000,1.500000,2.500000,0.950000,8.100000,8.100000,3.000000,0.000000,0.000000 point.3=2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-116.666667,0.000000,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.280151 static_cg_height=12.720257 [TurbineEngineData] fuel_flow_gain=0.002000 inlet_area=16.000000 rated_N2_rpm=29920.000000 static_thrust=35500.000000 afterburner_available=1 reverser_available=1 [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 use_no_default_pitch=1 use_no_default_bank=1 [Radios] // Radio Type=available, 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 [fuel] Center1=-21.000000,0.000000,0.000000,7680.000000,0.000000 Center2=-98.500000,0.000000,0.000000,3500.000000,0.000000 LeftMain=-54.200000,-14.600000,-4.500000,10170.000000,0.000000 RightMain=-54.200000,14.600000,-4.500000,10170.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=4262.000000 wing_span=83.833333 wing_root_chord=66.166667 wing_dihedral=0.000000 wing_incidence=0.247192 wing_twist=0.000000 oswald_efficiency_factor=0.903612 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=0.000000 htail_span=0.000000 htail_pos_lon=0.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=249.000000 vtail_span=17.991665 vtail_sweep=0.000000 vtail_pos_lon=-35.833333 vtail_pos_vert=5.833333 elevator_area=70.500000 aileron_area=26.800000 rudder_area=56.200000 elevator_up_limit=29.793805 elevator_down_limit=29.793805 aileron_up_limit=29.793805 aileron_down_limit=29.793805 rudder_limit=30.000070 elevator_trim_limit=19.996227 spoiler_limit=0.000000 spoilerons_available=1 aileron_to_spoileron_gain=3.000000 min_ailerons_for_spoilerons=9.969466 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=1 Engine.0=-38.000000,-19.250000,-1.000000 Engine.1=-38.000000,-15.250000,-1.000000 Engine.2=-38.000000,15.250000,-1.000000 Engine.3=-38.000000,19.250000,-1.000000 fuel_flow_scalar=1.000000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=59.388328,-1.307210,4.267655 [direction_indicators] direction_indicator.0=3,0 [Reference Speeds] flaps_up_stall_speed=120.000 full_flaps_stall_speed=90.000 cruise_speed=750.000 [Flaps.0] type=1 span-outboard=0.500 extending-time=8.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=2.500 pitch_scalar=0.500 flaps-position.0=0.000, 0.000 flaps-position.1=0.050, 0.000 flaps-position.2=0.100, 0.000 flaps-position.3=0.200, 0.000 flaps-position.4=0.400, 0.000 flaps-position.5=0.800, 0.000 flaps-position.6=1.000, 0.000 flaps-position.7=1.300, 0.000 flaps-position.8=2.000, 0.000