[fltsim.0]
title=L1011-100 Luftunternehme LTU
sim=tom1011
model=
panel=
sound=
texture=DL
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=D-AERA
atc_airline=LTU
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L1011-100
ui_variation=Luftunternehme LTU
ui_typerole=Kommerzielles Linienflugzeug
ui_createdby=
description=Широкофюзеляжный авиалайнер компании Локхид,обозначенный Локхид L-1011 Триcтар создавался в ответ на техническое задание компании Америкэн Эйрлайнз(American Airlines)на самолет малой и средней дальности и большой вместимости.Первый полет состоялся 17 ноября 1970г.Это был свободнонесущий низкоплан со стреловидным(35°)крылом,оснащенный тремя турбовентиляторными двигателями Роллс-Ройс(Rolls-Royce)RB.211 тягой 19051 кг(42000 фунтов).Вместимость составляла от двух до четырех членов экипажа и от 256 до 400 пассажиров.Первый контрольный полет был совершен авиакомпанией Истерн Эйр Лайнз(Eastern Air Lines)26 апреля 1972г.Выявились некоторые серьезные проблемы,в основном связанные с двигателями,но вскоре самолет ТриСтар завоевал популярность у авиакомпаний и любовь у пассажиров.

[fltsim.1]
title=L1011-100 British Airtours
sim=tom1011
model=
panel=
sound=
texture=British Airtours
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=G-BEAM
atc_airline=British Airtours
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L1011-100
ui_variation=British Airtours
ui_typerole=Commercial Airliner
ui_createdby=Thomas Ruth + Eric Cantu
description=Широкофюзеляжный авиалайнер компании Локхид,обозначенный Локхид L-1011 Триcтар создавался в ответ на техническое задание компании Америкэн Эйрлайнз(American Airlines)на самолет малой и средней дальности и большой вместимости.Первый полет состоялся 17 ноября 1970г.Это был свободнонесущий низкоплан со стреловидным(35°)крылом,оснащенный тремя турбовентиляторными двигателями Роллс-Ройс(Rolls-Royce)RB.211 тягой 19051 кг(42000 фунтов).Вместимость составляла от двух до четырех членов экипажа и от 256 до 400 пассажиров.Первый контрольный полет был совершен авиакомпанией Истерн Эйр Лайнз(Eastern Air Lines)26 апреля 1972г.Выявились некоторые серьезные проблемы,в основном связанные с двигателями,но вскоре самолет ТриСтар завоевал популярность у авиакомпаний и любовь у пассажиров.

[fltsim.2]
title=L1011-100 Eastern Airlines
sim=tom1011
model=
panel=
sound=
texture=Eastern Airlines
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N311EA
atc_airline=EASTERN
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L1011-100
ui_variation=Eastern Airlines
ui_typerole=Commercial Airliner
ui_createdby=Thomas Ruth + Eric Cantu
description=Широкофюзеляжный авиалайнер компании Локхид,обозначенный Локхид L-1011 Триcтар создавался в ответ на техническое задание компании Америкэн Эйрлайнз(American Airlines)на самолет малой и средней дальности и большой вместимости.Первый полет состоялся 17 ноября 1970г.Это был свободнонесущий низкоплан со стреловидным(35°)крылом,оснащенный тремя турбовентиляторными двигателями Роллс-Ройс(Rolls-Royce)RB.211 тягой 19051 кг(42000 фунтов).Вместимость составляла от двух до четырех членов экипажа и от 256 до 400 пассажиров.Первый контрольный полет был совершен авиакомпанией Истерн Эйр Лайнз(Eastern Air Lines)26 апреля 1972г.Выявились некоторые серьезные проблемы,в основном связанные с двигателями,но вскоре самолет ТриСтар завоевал популярность у авиакомпаний и любовь у пассажиров.

[fltsim.3]
title=L1011-100 TWA
sim=tom1011
model=
panel=
sound=
texture=TWA
kb_checklists=Boeing747-400_check
kb_reference=Boeing747-400_ref
atc_id=N31024
atc_airline=TWA
atc_flight_number=1123
atc_heavy=1
ui_manufacturer=Lockheed
ui_type=L1011-100
ui_variation=TWA (Trans World Airlines)
ui_typerole=Commercial Airliner
ui_createdby=Thomas Ruth + Eric Cantu
description=Широкофюзеляжный авиалайнер компании Локхид,обозначенный Локхид L-1011 Триcтар создавался в ответ на техническое задание компании Америкэн Эйрлайнз(American Airlines)на самолет малой и средней дальности и большой вместимости.Первый полет состоялся 17 ноября 1970г.Это был свободнонесущий низкоплан со стреловидным(35°)крылом,оснащенный тремя турбовентиляторными двигателями Роллс-Ройс(Rolls-Royce)RB.211 тягой 19051 кг(42000 фунтов).Вместимость составляла от двух до четырех членов экипажа и от 256 до 400 пассажиров.Первый контрольный полет был совершен авиакомпанией Истерн Эйр Лайнз(Eastern Air Lines)26 апреля 1972г.Выявились некоторые серьезные проблемы,в основном связанные с двигателями,но вскоре самолет ТриСтар завоевал популярность у авиакомпаний и любовь у пассажиров.


[General]
atc_type=LOCKHEED
atc_model=L1011
editable=1
performance=
Category=airplane

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

[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 = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.99, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Flight Engineer"
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 = .3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.78, 0.0, -0.849
InitialPbh=0, 0, 90

[CameraDefinition.003]
Title = "Jump Seat"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.14, 0.0, -0.77
InitialPbh=2, 0, 0


[CameraDefinition.0]
Title=Rechtes Seitenfenster
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Ansicht der rechten Tragflдche aus der Passagierkabine
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=Linkes Seitenfenster
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Ansicht der linken Tragflдche aus der Passagierkabine
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=Fahrwerk
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Ansicht des Fahrwerks und der Innenklappen der linken Tragflдche
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=Heck
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Ansicht nach vorn von einer Position hinter dem Luftfahrzeug
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=Rechte Tragflдche
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Ansicht von der rechten Tragflдchenspitze in Richtung Cockpit
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=Linke Tragflдche
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Ansicht von der linken Tragflдchenspitze in Richtung Cockpit
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


[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=467018                       // (pounds)
empty_weight=245949                           // (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=4440.0,	 0.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=2440.0,	 -50.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=3780.0,	  30.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=3140.0,	 -30.0,	 0.0,	 0.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Crew
station_name.1=Pax Fwd
station_name.2=Pax Mid
station_name.3=Pax Aft
station_name.4=Cargo Fwd
station_name.5=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, 8113, 460
LeftMain = -0.617, -20, 2, 8536, 481
RightMain = -0.617, 20, 2, 8536, 481

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 = 3460
wing_span = 155.35
wing_root_chord = 42.65
wing_dihedral = 5
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 = 255.39
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=4                                    // degrees
flaps-position.2=10                                    // degrees
flaps-position.3=22                                   // degrees
flaps-position.4=33                                   // 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=15                                  // 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 = 0, -35.65, -3.4,
engine.1 = -76, 0, 10,
engine.2 = 0, 35.65, -3.4,                 //(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=40140 
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)

point.0 = 1, 59.1928, 0, -12.1, 1200, 0, 1.6, 68, 0.9, 2, 0.7, 8, 9, 0, 180, 250
point.1 = 1, -12.3114, -18.2, -13.2, 1500, 1, 2.2, 0, 0.887, 2.5, 0.6, 9.9, 10.9, 2, 180, 250
point.2 = 1, -12.3114, 18.2, -13.2, 1500, 2, 2.2, 0, 0.887, 2.5, 0.6, 9.1, 10.1, 3, 180, 250
point.3 = 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.4 = 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.5 = 2, 61.8791, 0, -3.1502, 787, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 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.7 = 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.8 = 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


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 28
generator_alternator_voltage = 28
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,  24.59, -1.438, 15.57, fx_beaconh ,
light.1 = 1,  21.39,  1.438, 15.57, fx_beaconh ,
light.2 = 1,  6.345, -2.504, -4.682, fx_beaconb ,
light.3 = 1,  6.345,  2.504, -4.682, fx_beaconb ,
light.4 = 5,  30.92,  18.39,   2.68, fx_T332land  ,
light.5 = 5,  30.92, -18.39,   2.68, fx_T332land  ,
light.6 = 9, -75.81,   8.79,  28.61, fx_T332logo  ,
light.7 = 9, -75.81,  -8.79,  28.61, fx_T332logo  ,
light.8 = 4,  77.83,   0.00,   9.40, 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,  58.57, -7.12, 2.8, 0    ;Percent per second
exit.1 = 0.04,   -46.13,  7.50, -5.59, 1    ;Percent per second
exit.2 = 0.4,   -28.803, -8.540, -3.868, 2    ;Percent per second
exit.3 = 0.4,   -28.803, -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]		//Extends Landing light pods
tailhook_length=	4
tailhook_position=	0.0, 0.0, 0.0
cable_force_adjust=	0.5
[folding_wings]		//cargo doors and R2+L4 galley service doors
wing_fold_system_type=	4
fold_rates=		0.110,0.110