[fltsim.0] title=DC-10-30F DAS AIR CARGO sim=DC-10 model= panel= sound= texture=das atc_id=5X-JOE atc_airline=DAS atc_flight_number=8121 atc_parking_types=CARGO ui_manufacturer=Douglas ui_type=DC-10-30F ui_variation=DAS Air Cargo description=DAS Air Cargo McDonnell Douglas DC-10-30F. Ugandan registered Cargo Charter Aircraft. Textures by Nick Black. [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=Length: 200 ft. 10 in.\nWing span: 165 ft.\nWeight: 602,500 lbs MTOW\npwr: 3 GE CF6-80C2 turbofans @61,500 lbs\nStall: 130\/117\nOriginal: Bill Alderson\nMod's: Gary Carlson\nFlight Dynamics by Kevin Sison & Gary Carlson\nPanel and repainting in Alitalia livery by Capt. Italo D'Attomo atc_type=McDonnellDouglas atc_model=DC10 atc_heavy=1 [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=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 electric_pump=0 [airplane_geometry] wing_area=6470.000000 wing_span=231.833333 wing_root_chord=29.000000 wing_dihedral=6.998291 wing_incidence=0.000000 wing_twist=-3.999023 oswald_efficiency_factor=1.570486 wing_winglets_flag=1 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=1820.000000 htail_span=73.166667 htail_pos_lon=-102.500000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=1350.000000 vtail_span=41.892720 vtail_sweep=0.000000 vtail_pos_lon=-116.666667 vtail_pos_vert=5.833333 elevator_area=455.000000 aileron_area=268.720000 rudder_area=229.500000 elevator_up_limit=32.501974 elevator_down_limit=26.626481 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=1 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1, 87.42, 0.00, -18.00, 1181.1, 0, 4.521, 90.0, 1.63, 2.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0 point.1=1, -19.50, -12.00, -19.00, 1574.8, 1, 4.521, 0.0, 1.91, 2.5, 0.7470, 6.9, 6.9, 2, 0.0, 0.0 point.2=1, -19.50, 12.00, -19.00, 1574.8, 2, 4.521, 0.0, 1.91, 2.5, 0.7470, 7.1, 7.1, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = 0.10 static_cg_height = 17.56 gear_system_type=1 [GeneralEngineData] engine_type=1 Engine.0=17.333333,-25.333333,-7.000000 Engine.1=-77.500000,0.000000,21.833333 Engine.2=17.333333,25.333333,-7.000000 fuel_flow_scalar=1.000000 min_throttle_limit=-0.099915 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=77.695440 rated_N2_rpm=29920.000000 static_thrust=64746.200000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=140.000 full_flaps_stall_speed=112.000 cruise_speed=681.160 max_indicated_speed=350.000000 max_mach=0.879980 [keyboard_response] elevator=100.000000,200.000000 aileron=100.000000,200.000000 rudder=100.000000,200.000000 [Views] eyepoint=91.222728,-1.537894,4.126681 [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 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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 [brakes] toe_brakes_scale=0.350963 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=34.950426 flap_limit_idle=19.480565 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
