[fltsim.0] title=UNITED CARGO DC-10-30ER sim=DC1030ER_210 model= panel= sound= texture= checklists= description=Aircraft design and textures: FFG group & Kamal S. Kerba\nFlight dynamics: Hervé Sors\nCredits: Ron Freimuth, Prevair Group\n(C) Freeware Flight Group\nVersion 2.10\nREPAINT MASSIMO GRASSI ui_manufacturer=UNITED WORLDWIDE CARGO ui_type=DC10F ui_variation= atc_heavy=1 atc_id=UA atc_airline=UA atc_flight_number=335 [forcefeedback] 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=1300 ground_bumps_angle1=8900 ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 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 [General] performance=Engines: 3 x CF6-50C2 @ 51,800 lb each\nMTOW: 580,000 lb \s MLW: 421,000 lb\nFuel capacity: 41,413 USG (277,434 lb @ 6.7 lb\/USG)\nMax speed: 350 kts IAS or Mach 0.88\nFlaps settings: 5-15-20-25-30-35-50°\nMax operating altitude: 42,000 Ft\nTypical cruise setting: FL310-370 @ Mach 0.82\nRange with typical payload: 7,500 NM \n atc_type=UNITED atc_model=DC10F [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=0.000, 0.000, 0.000, 0.000 empty_weight= 302566.000 empty_weight_roll_MOI= 16400000.000 empty_weight_pitch_MOI= 29900000.000 empty_weight_yaw_MOI= 45100000.000 empty_weight_coupled_MOI= 451000.000 max_gross_weight= 580033.092 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 1.000, 0.000, 0.000, 14528.000, 3.000 Center2= 2.000, 0.000, 0.000, 14735.000, 3.000 LeftMain= -6.100, -27.600, 0.000, 6075.000, 3.000 RightMain= -6.100, 27.600, 0.000, 6075.000, 3.000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 4080.000 wing_span= 165.333 wing_root_chord= 24.667 wing_dihedral= 4.197 wing_incidence= 0.698 wing_twist= -1.494 oswald_efficiency_factor= 0.798 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 6.167 wing_pos_apex_vert= 0.000 htail_area= 1375.000 htail_span= 71.167 htail_pos_lon= -66.250 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 825.000 vtail_span= 32.749 vtail_sweep= 0.000 vtail_pos_lon= -57.917 vtail_pos_vert= 5.833 elevator_area= 45.000 aileron_area= 20.000 rudder_area= 50.000 elevator_up_limit= 26.001 elevator_down_limit= 26.001 aileron_up_limit= 26.001 aileron_down_limit= 26.001 rudder_limit= 26.001 elevator_trim_limit= 17.189 spoiler_limit= 59.989 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, 63.583, 0.000, -11.833, 1181.102, 0.000, 4.521, 75.780, 0.885, 2.500, 0.793, 10.000, 10.000, 0.000, 0.000, 0.000 point.1= 1.000, -8.750, -17.500, -11.833, 1574.803, 1.000, 4.521, 0.000, 0.899, 2.500, 0.469, 14.900, 14.900, 2.000, 0.000, 0.000 point.2= 1.000, -8.750, 17.500, -11.833, 1574.803, 2.000, 4.521, 0.000, 0.899, 2.500, 0.469, 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 [GeneralEngineData] engine_type= 1 Engine.0= 10.667, -26.833, -5.500 Engine.1= -69.500, 0.000, 17.333 Engine.2= 10.667, 26.833, -5.500 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 87.000 rated_N2_rpm= 29920.000 static_thrust= 51800.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 170.000 full_flaps_stall_speed= 136.000 cruise_speed= 497.985 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=86.250205,-1.486631,7.830442 [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= 20.000 system_type= 1 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= 7.143, 0.000 flaps-position.2= 14.286, 0.000 flaps-position.3= 21.429, 0.000 flaps-position.4= 28.571, 0.000 flaps-position.5= 35.714, 0.000 flaps-position.6= 42.857, 0.000 flaps-position.7= 50.000, 0.000