[fltsim.0] title=DC-10-40ER American Airlines sim=dc-10-40er model= panel= sound= texture= checklists= kb_checklists= kb_reference= description= ui_manufacturer=McDonnell Douglas ui_type=DC10-40 ui_variation=American Airlanes atc_heavy=1 atc_id= atc_airline=American atc_flight_number=1234 visual_damage=1 [General] performance=Length: 180 ft. 8 in\nWing span: 165 ft. 4 in\nHeight: 58ft. 1 in.\nDry Weight: 326,434 lbs\nMGTOW: 572,000 lbs.\nMLW: 411,000 lbs (84,566 lbs fuel)\nPower: 3 PW JT9D-59A (53,000lbs ST)\nFuel: 37,198 Gal (245,566 lbs)\nRange: 4,100 Miles (28K lbs\/hr)\nPAX: 250-380\nTypical Cruise: M0.83 (490 knots gs)\nTake-off distance (MTOW): 10,000ft\nLand Distance (MLW): 5,960 ft.\nFS2K2 Only Dynamics by: Alejandro Villa March 9, 2002 atc_type=MCDONNELDOUGLAS atc_model=DC10-30 editable=0 [ground_reaction] max_steering_angle=45 ;Voltage of the battery when fully charged. In Volts: max_battery_voltage=28 ;The voltage produced by the alternator/generator, in Volts: generator_alternator_voltage=28 max_generator_alternator_amps=90 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4): fuel_transfer_pump=0, 5, 24.0 flap_motor=0, 15, 24.0 gear_motor=0, 15, 24.0 autopilot=0, 5, 24.0 avionics_bus=0, 5, 24.0 avionics=1, 10, 24.0 pitot_heat=0, 15, 24.0 additional_system=0, 20, 24.0 gear_warning=0, 2, 24.0 fuel_pump=3, 10, 24.0 starter1=0, 20, 24.0 starter2=0, 20, 24.0 starter3=0, 20, 24.0 light_nav=2, 2, 24.0 marker_beacon=2, 2, 24.0 light_beacon=2, 2, 24.0 light_landing=2, 5, 24.0 light_taxi=2, 5, 24.0 light_strobe=2, 5, 24.0 light_panel=2, 2, 24.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=100.000 pitch_takeoff_ga=10.000 use_no_default_pitch=1 use_no_default_bank=1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1,1 Com.2=1,1 Nav.1=1,0,1 Nav.2=1,0,0 Adf.1=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] // Vertical, Longitude, latitude: smoke.1=-9.033, -21.833, -29.167, fx_smoke_rx smoke.0=20.000, -110.000, 0.000, fx_smoke_rx smoke.2=-9.033, -21.833, 29.167, fx_smoke_rx [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [LIGHTS] light.0=2, -78.000, 0.000, 47.100, fx_strobeh , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=200000.000000 empty_weight_roll_MOI=8177792.000000 empty_weight_pitch_MOI=16030000.000000 empty_weight_yaw_MOI=15016444.000000 empty_weight_coupled_MOI=1300.000000 [fuel] LeftMain=0.000000,0.000000,0.000000,10000.000000,0.000000 RightMain=0.000000,0.000000,0.000000,10000.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=3447.000000 wing_span=155.333333 wing_root_chord=22.166667 wing_dihedral=5.498657 wing_incidence=0.000000 wing_twist=-0.999756 oswald_efficiency_factor=1.875505 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=1214.000000 htail_span=71.583333 htail_pos_lon=-66.666667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=920.000000 vtail_span=34.583233 vtail_sweep=0.000000 vtail_pos_lon=-66.666667 vtail_pos_vert=5.833333 elevator_area=303.500000 aileron_area=137.880000 rudder_area=156.400000 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=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000, 63.583, 0.000, -11.833, 1181.102, 0.000, 4.466, 75.780, 0.873, 2.500, 0.798, 10.000, 10.000, 0.000, 0.000, 0.000 point.1=1.000, -8.750, -17.500, -11.833, 1574.803, 1.000, 4.466, 0.000, 0.887, 2.500, 0.473, 14.900, 14.900, 2.000, 0.000, 0.000 point.2=1.000, -8.750, 17.500, -11.833, 1574.803, 2.000, 4.466, 0.000, 0.887, 2.500, 0.473, 15.100, 15.100, 3.000, 0.000, 0.000 point.3=2.000, -43.667, -82.667, 4.417, 787.402, 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, -43.667, 82.667, 4.417, 787.402, 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, -77.833, 0.000, 6.083, 787.402, 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, 64.917, 0.000, 6.083, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=11.414 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=4.999057,0.000000 flaps-position.2=9.998114,0.000000 flaps-position.3=14.997170,0.000000 flaps-position.4=19.996227,0.000000 flaps-position.5=24.995284,0.000000 flaps-position.6=29.994341,0.000000 flaps-position.7=34.993397,0.000000 flaps-position.8=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=3.333333,32.500000,6.333333 Engine.1=-76.416667,0.000000,-7.916667 Engine.2=3.333333,-32.500000,6.333333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=51.095520 rated_N2_rpm=29920.000000 static_thrust=42579.600000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=160.000000 full_flaps_stall_speed=128.000000 cruise_speed=788.271904 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=78.496658,0.000000,3.998524 [direction_indicators] direction_indicator.0=3,0