[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