[fltsim.0]
title=Douglas C-124 C Utah Air Guard 2
sim=C-124-2
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Douglas
ui_type=C-124 C
ui_variation=Utah Air Guard 2
description=Douglas C-124 C Globemaster II, USAF,\nUAG (Utah Air Guard),\nregistration 0-20976, \nwas used at the begining of the seventies.\nVersion: AP 1.2a  \n\n\n\n\n
atc_heavy=0
atc_id=20976
atc_airline=AIR FORCE
atc_flight_number=20976

[General]
performance=Wing span: 53.09 m (174.18 ft)\nLength: 39.62 m (129.99 ft)\nWeight: 88225 kg (max)\nPower:4x 3853 HP \/ 2833 kW \nP&W R-4360-63A\nSpeed: 436 km\/h (271 mph)\n\nBase design & Textures: \nArik Hohmeyer\n\nComplete rework with FSDS2:\nChris Grabow\n\nFlightdynamic: \nbased on Dave McQueen's C-97 file, \nmodified by Wolfram Beckert\n\nDate: February 2003, \nModel version AP 1.2\n\nFS-DESIGN BERLIN\n(c) 2001-2003 FREEWARE\nwww.fsdesign-berlin.da.ru\n\n\n\n
atc_type=MCDONNELDOUGLAS
atc_model=C124

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[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=94000.000
empty_weight_roll_MOI=1066725.000
empty_weight_pitch_MOI=1417509.000
empty_weight_yaw_MOI=1786469.000
empty_weight_coupled_MOI=0.000
max_gross_weight=128540.000
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
LeftMain=0.000, 0.000, 0.000, 3095.000, 0.000
LeftAux=0.000, -56.417, 0.000, 0.000, 0.000
RightMain=0.000, 0.000, 0.000, 3095.000, 0.000
RightAux=0.000, 56.417, 0.000, 0.000, 0.000
fuel_type=1.000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=1726.000
wing_span=141.250
wing_root_chord=12.250
wing_dihedral=4.499
wing_incidence=2.500
wing_twist=-1.000
oswald_efficiency_factor=0.876
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=344.000
htail_span=43.000
htail_pos_lon=-59.583
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=329.000
vtail_span=20.681
vtail_sweep=0.000
vtail_pos_lon=-43.333
vtail_pos_vert=1.500
elevator_area=147.920
aileron_area=172.600
rudder_area=115.150
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=26.491
elevator_trim_limit=19.481
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

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.4
induced_drag_scalar=1.3
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.1
pitch_stability=1.4
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[contact_points]
point.0=1.000, 29.667, 0.000, -8.417, 1574.803, 0.000, 1.391, 48.000, 0.297, 2.500, 0.651, 15.000, 15.000, 0.000, 0.000, 0.000
point.1=1.000, -4.333, -15.000, -7.417, 1574.803, 1.000, 1.391, 0.000, 0.297, 2.500, 0.651, 15.000, 15.000, 2.000, 0.000, 0.000
point.2=1.000, -4.333, 15.000, -7.417, 1574.803, 2.000, 1.391, 0.000, 0.297, 2.500, 0.651, 15.000, 15.000, 3.000, 0.000, 0.000
point.3=2.000, 37.437, 0.003, -1.613, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.4=2.000, -62.601, 0.030, 3.464, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.5=2.000, -5.102, 86.220, 7.933, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.6=2.000, -4.446, -85.836, 8.261, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.7=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.8=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.9=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.10=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.11=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.12=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.13=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.14=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.15=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.16=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.17=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.18=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.19=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.20=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.21=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.22=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.23=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.24=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.25=23.94, 0.03, -8.70, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.26=-7.50, -17.97, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
point.27=-7.31, 17.40, -8.17, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 4.0, 4.0, 0
static_pitch=0.976
static_cg_height=8.436

[GeneralEngineData]
engine_type=0
Engine.0=10.000, -38.000, 3.000
Engine.1=10.833, -18.000, -1.267
Engine.2=10.833, 18.000, -1.267
Engine.3=10.000, 38.000, 3.000
fuel_flow_scalar=1.000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=0.950
idle_rpm_mechanical_efficiency_scalar=1.40
max_rpm_friction_scalar=1.050
idle_rpm_friction_scalar=0.650
cylinder_displacement=251.000
compression_ratio=8.000
number_of_cylinders=24
max_rated_rpm=2600.000
max_rated_hp=3850.000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300
turbocharged=0
max_design_mp=0.000
min_design_mp=0.000
critical_altitude=0.000
emergency_boost_type=0
emergency_boost_mp_offset=0.000
emergency_boost_gain_offset=0.000
fuel_air_auto_mixture=0
auto_ignition=0

[propeller]
propeller_type=0
propeller_diameter=16.667
propeller_blades=3
propeller_moi=98.528
beta_max=65.000
beta_min=15.000
min_gov_rpm=1400.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=20.000
low_speed_theory_limit=80.000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000
beta_feather=0.000
power_absorbed_cf=0.000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000

[Reference Speeds]
flaps_up_stall_speed=92.000
full_flaps_stall_speed=72.000
cruise_speed=321.000

[keyboard_response]
elevator=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000

[Views]
eyepoint=32.796, 0.000, 7.395

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000
autothrottle_available=1
pitch_takeoff_ga=8.000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[direction_indicators]
direction_indicator.0=1,0

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=2,   -5.1, -88.5,  10.1, fx_strobe ,
light.1=2,   -5.1,  88.5,  10.1, fx_strobe ,
light.2=4, 39.55,  0.00,16.21, fx_vclight

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.200
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=9.998, 0.000
flaps-position.2=19.996, 0.000
flaps-position.3=29.994, 0.000
flaps-position.4=39.992, 0.000