[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