[fltsim.0]
title=Dc10-30 CARGO LONGFAIRING HSTABFAIRING VSTABFAIRING KC10
sim=tomdc10
model=
panel=
sound=
texture=USAFgrey
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=60035
atc_airline=USAF
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=McDonnell Douglas
ui_type=KC-10A Extender
ui_variation=US Air Force
ui_typerole=Kommerzielles Linienflugzeug
ui_createdby=Thomas Ruth + Eric Cantu
description=McDonnell Douglas KC-10A Extender—американский самолёт-заправщик,созданный на базе гражданского авиалайнера DC-10.Используется ВВС США наряду с более старыми KC-135.На вооружении Королевских ВВС Нидерландов имеются два самолёта KDC-10,представляющие собой переоборудованные DC-10.По своим характеристикам KC-10 предназначен в первую очередь для взаимодействия с тактической авиацией.

[General]
atc_type=MD
atc_model=DC10
editable=1
performance=
Category=airplane

[CameraDefinition.0]
Title=Left wingview
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Left trailing edge as seen from paxcabin
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=-3.318, 3.15, -11.35
InitialPbh=5, 0, 270
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Right wingview
Guid={D368D3EA-21FB-4d88-97BC-771106DCC59B}
Description=Right trailing edge as seen from paxcabin
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=3.318, 3.15, -11.35
InitialPbh=5, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Left engine view
Guid={E4F8DA49-C99E-40ae-8467-AC874BB497B6}
Description=Left engine as seen from flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=-2.514, 3.14, 25.44
InitialPbh=5, 0, 210
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Right engine view
Guid={C3CD1BAC-B511-4557-B3CE-C5F6EAD00807}
Description=Right engine as seen from flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=2.514, 3.14, 25.44
InitialPbh=5, 0, 150
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Main gear cam
Guid={D1EE9F66-E2A5-4dd8-9874-D87E96E1F980}
Description=Main gear as seen from the belly fairing
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=0, -1.51, -9.67
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.5]
Title=Nose gear cam
Guid={5D9AC711-EC3E-4e47-AF27-820DE14AF3E1}
Description=Runway as seen from the nose gear
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
ShowWeather=Yes
InitialXyz=0, -1.29, 20.96
InitialPbh=0, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.6]
Title=Tail cam
Guid={665E785E-73B0-44e7-89F6-229E1F6BA1C9}
Description=Aircraft as seen from the tip of the vertical stabilizer
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.3
ShowWeather=Yes
InitialXyz=0, 15.62, -24.94
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.001]
Title=Right Seat
Guid={8ff6c134-098d-409f-baec-caba3f683f98}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.7
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.0, 0.0, 0.0
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title=Visitor at Cockpit Door
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.7
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.60, -1.2
InitialPbh=2, 0, 0


[CameraDefinition.003]
Title=Flight Engineer
Guid={609b24ab-a96c-46d9-a572-29f8cb15547b}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.4
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.9, 0.00, -1.0
InitialPbh=12, 00, 90



[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.0    //Scalar on heat effectiveness, 0 = not available


[WEIGHT_AND_BALANCE]
max_gross_weight=593000                       // (pounds)
empty_weight=241027                           // (pounds)

reference_datum_position=0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-5, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=480.0,	 50.0,	-2.0,	 8.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=2440.0,	  50.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=2440.0,	 -50.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)


station_name.0=Crew
station_name.1=Cargo Fwd
station_name.2=Cargo Aft


;Moments of Inertia
empty_weight_roll_MOI=2834360.42
empty_weight_pitch_MOI=9373091.43
empty_weight_yaw_MOI=13353909.19
empty_weight_coupled_MOI=0


[fuel]
Center1 = -18.5, 0, -2.7, 9700, 260
Center2 = -18.5, 0, -2.7, 14600, 260 // -15Series with bigger Centertank, -30 and -40 with both Centertanks
LeftMain = -0.617, -20, 2, 6000, 281
RightMain = -0.617, 20, 2, 6000, 281
Center3 = 0, 0, -2.7, 7020, 90

fuel_type=2                                     //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=3
electric_pump=3
fuel_dump_rate=0.0167                        //Percent of max quantity per second, i.e. about 1 minute for full fuel

[airplane_geometry]
wing_area = 3958
wing_span = 165.4
wing_root_chord = 42.65
wing_dihedral = 7.58
wing_incidence = 0.00
wing_twist = -0.50
oswald_efficiency_factor = 0.81
wing_winglets_flag = 0
wing_sweep = 35
wing_pos_apex_lon = 20
wing_pos_apex_vert = 0
htail_area = 1282.02
htail_span = 71.83
htail_pos_lon = -50.68
htail_pos_vert = 7.5
htail_incidence = 0.00
htail_sweep = 35
vtail_area = 550.05
vtail_span = 32.47
vtail_sweep = 40
vtail_pos_lon = -52.40
vtail_pos_vert = 11.76
elevator_area = 1282.02
aileron_area = 265.39
rudder_area = 161.00
elevator_up_limit = 26.00
elevator_down_limit = 20.00
aileron_up_limit = 30.00
aileron_down_limit = 30.00
rudder_limit = 33.00
elevator_trim_limit = 24.00
spoiler_limit = 60.00
aileron_to_spoileron_gain = 1.00
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 1.00
min_flaps_for_spoilerons = 0
spoilerons_available = 1
auto_spoiler_available=1
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
load_safety_factor=1.5               //Design G load safety factor

[Reference Speeds]
flaps_up_stall_speed=192.0                 //Knots True (KTAS)
full_flaps_stall_speed=130.0                 //Knots True (KTAS)
cruise_speed=600.0                 //Knots True (KTAS)
max_mach=0.88
max_indicated_speed=360.0                 //Red line (KIAS)

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=20                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=0                                    // degrees
flaps-position.2=15                                    // degrees
flaps-position.3=22                                   // degrees
flaps-position.4=35                                   // degrees
flaps-position.5=50                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=280                                  // KIAS
lift_scalar=0.45
drag_scalar=0.8
pitch_scalar=0.3
system_type=1                                         //Hydraulic

[flaps.1]
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=10                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=15                                    // degrees
flaps-position.2=15                                    // degrees
flaps-position.3=15                                   // degrees
flaps-position.4=25                                  // degrees
flaps-position.5=25                                  // degrees
damaging-speed=250                                  // KIAS
blowout-speed=280                                  // KIAS
lift_scalar=0.2
drag_scalar=0.2
pitch_scalar=0.2
system_type=1                                         //Hydraulic

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

[GeneralEngineData]
engine_type=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 = 13.52, -29.244, -2.75,
engine.1 = -79, 0, 22.61,
engine.2 = 13.52, 29.244, -2.75,                 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.77                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.3;                     //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
bypass_ratio=		4.3
fuel_flow_gain=0.0010 
inlet_area=29.928 
rated_N2_rpm=10611 
static_thrust=52500 
afterburner_available=0 
reverser_available=1                     //Thrust reverser available?
ThrustSpecificFuelConsumption=0.40

[jet_engine]
thrust_scalar=1.0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=96.5
autothrottle_takeoff_ga=1
use_no_default_pitch=			1
use_no_default_bank=			1
pitch_takeoff_ga=18;
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.0
max_pitch_acceleration=3.0
max_pitch_velocity_lo_alt=4.0
max_pitch_velocity_hi_alt=2.9
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=2.0
max_bank_velocity=3.00
max_throttle_rate=0.2
nav_proportional_control=12.00
nav_integrator_control=			0.05
nav_derivative_control=			0.01
nav_integrator_boundary=		0.5
nav_derivative_boundary=		0.35
gs_proportional_control=		10.0
gs_integrator_control=			0.50
gs_derivative_control=			0.00
gs_integrator_boundary=			0.7
gs_derivative_boundary=			0.00
yaw_damper_gain=			1.00

[contact_points]

;/0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
;/1  Longitudinal Position        (feet)
;/2  Lateral Position             (feet)
;/3  Vertical Position            (feet)
;/4  Impact Damage Threshold      (Feet Per Minute)
;/5  Brake Map                    (0=None, 1=Left, 2=Right)
;/6  Wheel Radius                 (feet)
;/7  Steer Angle                  (degrees)
;/8  Static Compression           (feet)  (0 if rigid)
;/9  Max/Static Compression Ratio
;/10 Damping Ratio                (0=Undamped, 1=Critically Damped)
;/11 Extension Time               (seconds)
;/12 Retraction Time              (seconds)
;/13 Sound Type
;/14 Airspeed limit for retraction     (KIAS)
;/15 Airspeed that gear gets damage at (KIAS)
;         0      1       2        3     4    5    6   7   8      9    10    11    12    13  14    15
;----------------------------------------------------------------------------------------------------
point.0 = 1,  67.155,    0,    -12.38, 1200, 0, 1.68, 65, 0.590, 3.361, 0.72,    8,    9,   0, 180, 250
point.1 = 1, -12.3114, -18.2,  -12.38, 1500, 1, 2.51,  0, 0.590, 2.849, 0.74,  9.9, 10.9,   2, 180, 250
point.2 = 1, -12.3114,  18.2,  -12.38, 1500, 2, 2.51,  0, 0.590, 2.849, 0.74,  9.1, 10.1,   3, 180, 250
point.3 = 1, -12.3114,  0.00,  -12.38, 1500, 2, 2.51,  0, 0.590, 2.849, 0.74,  9.1, 10.1,   3, 180, 250 //AUX Gear
point.4 = 2, -34.00,   -86.00,   8.40,  787, 0, 0.0,   0, 0.000, 0.0, 0.0,  0.0,  0.0,   5,   0,   0
point.5 = 2, -34.00,    86.00,   8.40,  787, 0, 0.0,   0, 0.000, 0.0, 0.0,  0.0,  0.0,   6,   0,   0
point.6 = 2,  61.8791,   0,   -3.1502,  787, 0, 0.0,   0, 0,       0,   0,    0,    0,   9,   0,   0
point.7 = 2, -93.50,     0.00,  25.00,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0,   4,   0,   0
point.8 = 2, -85.50,     0.00,  11.50,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0,   4,   0,   0
point.9 = 2, -46.50,     0.00,  -1.65,  787, 0, 0.0,  0, 0.000, 0.0, 0.0,  0.0,  0.0,   4,   0,   0
                                     
static_pitch=0.0
static_cg_height=12.5
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=5.0     //Flap angle that activates warning at idle
flap_limit_power=25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1        //Parking brake available
toe_brakes_scale=0.599  //Brake scalar
auto_brakes=4
hydraulic_system_scalar=1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure

[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=0         //no electric pumps
engine_map=1,1,1,0   //pumps on Eng1,2,3,4

[Views]
eyepoint=89.1, -1.76, 11.34              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 130
generator_alternator_voltage = 115
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1
electric_always_available = 0
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 15, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
starter3 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
fuel_transfer_pump = 0, 5, 17


[Radios]
;/ Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
light.0 = 1,  -0.90,   0.00, 18.70, fx_beaconh ,
light.1 = 1,  -30.90,   0.00, -3.00, fx_beaconb ,
light.2 = 5,  80.92,  18.39,  -3.38, fx_T332land  ,
light.3 = 5,  80.92, -18.39,  -3.38, fx_T332land  ,
//light.4 = 9, -75.81,   8.79,  28.61, fx_T332logo  ,
//light.5 = 9, -75.81,  -8.79,  28.61, fx_T332logo  ,
light.6 = 10,  88.00,   0.00,  11.3, fx_vclighth  ,

[direction_indicators]
;/1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
;/2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1

[attitude_indicators]
;/Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1

[altimeters]
altimeter.0=1
altimeter.1=1

[turn_indicators]
;/Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0

[vacuum_system]
;/Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=4.500000
engine_map=1,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[keyboard_response]
;/Breakpoint speeds (knots) on the keyboard increments of control surfaces.
;/Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator = 100, 200
aileron = 100, 200
rudder = 100, 200

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

[exits]
number_of_exits = 4
exit.0 = 0.4,  78.83, -8.02, 12.65, 0    ;Percent per second
exit.1 = 0.04,   -36.80,  7.09, 0.19, 1    ;Percent per second
exit.2 = 0.06,   8.803, -8.540, 3.868, 2    ;Percent per second
exit.3 = 0.05,   8.803, -8.540, 3.868, 2    ;Percent per second

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[stall_warning]
type=1
stick_shaker=1

[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots

[TailHook]		//KC10 Refueling Boom
tailhook_length=	4
tailhook_position=	0.0, 0.0, 0.0
cable_force_adjust=	0.5