; Localized	10/09/2007 09:20 PM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Boeing 747-400 Paint1
sim=Boeing747-400
model=""
panel=""
sound=""
texture=1
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747K
atc_airline=Boeing
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Боинг-стандарт
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.1]
title=Boeing 747-400 Paint2
sim=Boeing747-400
model=""
panel=""
sound=""
texture=2
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747I
atc_airline=World Travel
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Ворлд Трэвел Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.2]
title=Boeing 747-400 Paint4
sim=Boeing747-400
model=""
panel=""
sound=""
texture=4
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747P
atc_airline=Orbit
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Орбит Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.3]
title=Boeing 747-400 Paint5
sim=Boeing747-400
model=""
panel=""
sound=""
texture=5
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747I
atc_airline=Pacifica
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Пасифика Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.4]
title=Boeing 747-400 Paint8
sim=Boeing747-400
model=""
panel=""
sound=""
texture=8
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747I
atc_airline=Global Freight
atc_flight_number=1123
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Глобал Фрейтвэйс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.5]
title=Boeing 747-400 Paint9
sim=Boeing747-400
model=""
panel=""
sound=""
texture=9
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747I
atc_airline=Mothball
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Списанный
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.6]
title=Boeing 747-400
sim=Boeing747-400
model=""
panel=""
sound=""
texture=""
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N747
atc_airline=""
atc_flight_number=1123
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=Белый
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Более 30 лет назад "Боинг-747" совершил свой первый рейс из Нью-Йорка в Лондон, став с тех пор новым стандартом для больших пассажирских самолетов. Скорость, дальность и грузоподъемность "Боинга-747" были и остаются лучшими в своем классе.

[fltsim.7]
title=Boeing 747-400 Paint10
sim=Boeing747-400
model=""
panel=""
sound=""
texture=3
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=EV-251
atc_airline=BELAVIA
atc_flight_number=PA167
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Боинг
ui_type=747-400
ui_variation=БЕЛАВИА
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description=Все больше и больше набирает силу Беларусская Авиа-компания БЕЛАВИА и на смену изношенным Ту-шкам приходят мощные современные Боинги

[General]
atc_type=BOEING
atc_model=B744
editable=0
performance=Крейсерская скорость: М 0,85 (565 миль/ч, или 910 км/ч)\n\nДвигатели: Pratt & Whitney PW4062: Rolls-Royce RB211-524H, General Electric CF6-80C2B5F\n\nМаксимальная дальность: 7325 м. миль (13570 км)\n\nПрактический потолок: 45100 фт. (13747 м)\n\nЗапас топлива: 57285 галл. (216840 л)\n\nВес без груза: 394088 фнт. (178755 кг)\n\nМаксимальный вес 875000 фнт. (396893 кг)\n\nДлина: 231 фт. 10 д. (70,6 м)\n\nРазмах крыла: 211 фт. 5 д. (64,4 м)\n\nВысота: 63 фт. 8 д. (19,4 м)\n\nПосадочных мест:\nв конфигурации 3 класса - 416\nв конфигурации 2 класса - 524
Category=airplane

[CameraDefinition.0]
Title=Окно справа
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Вид на правое крыло из пассажирской кабины
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=5.5, 0.75, -13
InitialPbh=0, 0, 95
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Окно слева
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Вид на левое крыло из пассажирской кабины
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=-5.5, 0.75, -13
InitialPbh=0, 0, 265
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Шасси
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Вид от шасси и левых закрылков
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.58
ShowWeather=Yes
InitialXyz=-11, -4.1, -16
InitialPbh=0, 0, 44
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Хвост
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Вид с хвостовой части самолета
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 9.0, -80.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Правое крыло
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Вид на кабину с кончика правого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=40.8, 1.4, 4.0
InitialPbh=6, 0, 270
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title=Левое крыло
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Вид на кабину с кончика левого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-40.8, 1.4, 4.0
InitialPbh=6, 0, 90
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMode=Minimum

[CameraDefinition.001]
Title=Правое сиденье
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=.75
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.25, 0.0, 0.0
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title=Блок радиосвязи
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.30, -0.05
InitialPbh=85, 0, 0

[CameraDefinition.003]
Title=Верхняя приборная панель
Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.8
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.635, -0.58, -0.2
InitialPbh=-55.0, 0, 0

[CameraDefinition.004]
Title=Панель управления двигателем
Guid={195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.6, 0.3, 0
InitialPbh=59.5, 0, 0


[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=875000                       // (pounds)
empty_weight=394088                           // (pounds)

reference_datum_position=83.5, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-90.5, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170.0,	 -19.0,	-2.0,	 8.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170.0,	 -19.0,	 2.0,	 8.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=1700.0,	 -83.5,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=5440.0,	 -27.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=5780.0,	 -65.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=7140.0,	 -50.0,	 0.0,	 8.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=10710.0,	 -91.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=18020.0,	-119.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=23800.0,	-160.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9=18000.0,	 -52.0,	 0.0,	-6.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10=6000.0,	-123.0,	 0.0,	-6.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Пилот
station_name.1=2-й пилот
station_name.2=Экипаж
station_name.3=1-й класс
station_name.4=Бизнес-класс
station_name.5=Верхняя палуба
station_name.6=Тур. кл. 1-7
station_name.7=Тур. кл. 8-18
station_name.8=Тур. кл. 19-34
station_name.9=Баг. отсек (П)
station_name.10=Баг. отсек (З)

;Moments of Inertia
empty_weight_roll_MOI=13352310
empty_weight_pitch_MOI=24223159
empty_weight_yaw_MOI=39531785
empty_weight_coupled_MOI=0


[fuel]
LeftMain=-96.0, -28.0, -4.0, 12546.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-96.0,  28.0, -4.0, 12546.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-112.0, -36.5, -3.0,  4482.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-112.0,  36.5, -3.0,  4482.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip=-130.0, -73.0,  0.0,  1322.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip=-130.0,  73.0,  0.0,  1322.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1=-83.5,   0.0, -7.0, 17164.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=-193.5,   0.0,  6.0,  3300.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

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

[airplane_geometry]
wing_area=5825.0                //Square feet
wing_span=211.4                 //Feet
wing_root_chord=48.8                  //Feet
wing_dihedral=7.0                   //Degrees
wing_incidence=2.0                   //Degrees
wing_twist=-1.0                  //Degrees
oswald_efficiency_factor=0.68                  //Measure of lift effeciency of wing
wing_winglets_flag=1                     //Are winglets available?
wing_sweep=37.5                  //Degrees, wing leading edge
wing_pos_apex_lon=-58.2                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=-5                     //Feet, vertical distance from reference point, positive going up
htail_area=1470                  //Square feet
htail_span=72.8                  //Feet
htail_pos_lon=-210.0                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0                   //Degrees
htail_sweep=37.5                  //Degrees, horizontal tail leading edge
vtail_area=1060                  //Square feet
vtail_span=37.1                  //Feet, tip to body
vtail_sweep=45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-198.5                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=26.1                  //Feet, vertical distance from reference point, positive going up
elevator_area=327                   //Square feet
aileron_area=225                   //Square feet
rudder_area=230                   //Square feet
elevator_up_limit=25                    //Degrees
elevator_down_limit=15                    //Degrees
aileron_up_limit=25                    //Degrees
aileron_down_limit=15                    //Degrees
rudder_limit=31.5                  //Degrees
elevator_trim_limit=20                    //Degrees
spoiler_limit=45                    //Degrees
spoiler_extension_time=2.0			//Seconds
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
positive_g_limit_flaps_up=4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=3.0               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up=-3.0               //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-2.0               //Design G load tolerance (negative, flaps down)
load_safety_factor=1.5               //Design G load safety factor

[Reference Speeds]
flaps_up_stall_speed=140.0                 //Knots True (KTAS)
full_flaps_stall_speed=112.0                 //Knots True (KTAS)
cruise_speed=505.0                 //Knots True (KTAS)
max_mach=0.92
max_indicated_speed=365.0                 //Red line (KIAS)

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=25                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=1                                    // degrees
flaps-position.2=5                                    // degrees
flaps-position.3=10                                   // degrees
flaps-position.4=20                                   // degrees
flaps-position.5=25                                   // degrees
flaps-position.6=30                                   // degrees
damaging-speed=200                                  // KIAS
blowout-speed=250                                  // KIAS
lift_scalar=0.7
drag_scalar=0.9
pitch_scalar=0.9
system_type=1                                         //Hydraulic

[flaps.1]
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=2                                    // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=1.0                                  // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.3
drag_scalar=0.1
pitch_scalar=0.1
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=-107.5, -69.5,  -6.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-76.0, -38.9, -10.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2=-76.0,  38.9, -10.4                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3=-107.5,  69.5,  -6.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0                   //Scalar for fuel flow efficiency
min_throttle_limit=-0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain=0.002                 //Gain on fuel flow
inlet_area=60.0                  //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=56750                 //Lbs, max rated static thrust at Sea Level
afterburner_available=0                     //Afterburner available?
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=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=99
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.05
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=18.0
gs_integrator_control=0.33
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0

[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)

point.0=1,  -25.0,     0.0, -17.2, 1600, 0, 2.0, 70.0, 0.5, 3.5, 0.900,  9.0,  8.0, 0, 220, 250
point.1=1, -114.0,   -18.0, -20.0, 1600, 1, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0,  9.0, 2, 220, 250
point.2=1, -114.0,    18.0, -20.0, 1600, 2, 2.0, 13.0, 3.0, 2.5, 0.900, 11.0,  9.0, 3, 220, 250
point.3=2, -152.6,  -103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
point.4=2, -152.6,   103.5,   3.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
point.5=2,    3.0,     0.0,   0.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
point.6=2, -222.7,     0.0,   4.0, 1000, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
                                     
static_pitch=0.0
static_cg_height=17.0
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=1.24  //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=1,1,1,1   //pumps on Eng1,2,3,4

[Views]
eyepoint=-18.55, -2.0, 11.0              ; 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)
autopilot=0, 5 , 17.0
avionics_bus=0, 5 , 17.0
avionics=1, 5 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0


[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.1=3, -223.85,    0.00,   8.85, fx_navwhih ,
light.2=2, -228.97,    0.00,  44.62, fx_strobeh ,
light.3=1,  -45.05,    0.00,  15.65, fx_beaconh ,
light.4=1,  -80.22,    0.00, -11.05, fx_beaconb ,
light.5=4,  -18.24,    0.00,  11.19, 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=2
attitude_indicator.1=2

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

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

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

[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=150, 250
aileron=150, 250
rudder=150, 250

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

[exits]
number_of_exits=2
exit.0=0.4, -30.30,  -9.0,  0.88,0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1=0.4, -146.0,   8.0, -7.5, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2=0.4, -42.30,   9.0, -7,   2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

[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=2
stick_shaker=1

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