; Localized	09/12/2006 03:16 AM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Antonov AN-225 Sovjet Air Force
sim=an225
model=BURAN
panel=
sound=
texture=BURAN
kb_checklists=
kb_reference=
description=The Anotonov-225 "MRIYA/DREAM". This one is the biggest and heaviest aircraft flying on Earth. She was designed to carry the Soviet space shuttle "Buran/Snowstorm". After spending years of inactivity at Kiev Airport after the Buran program was canceled, she was put back into service in 2001 to assist her smaller sister an124. This paint scheme shows her colours when carrying Buran.
ui_manufacturer=Antonov
ui_type=AN225
ui_variation=Sovjet Air Force
ui_typerole=Heavy Freighter
ui_createdby=Tom
atc_heavy=1
atc_id=82005
atc_airline=AEROFLOT
atc_parking_types=CARGO,MIL_CARGO,RAMP 
atc_flight_number=8266

[fltsim.1]
title=Antonov AN-225 Antonov 2009
sim=an225
model=PLAIN
panel=
sound=
texture=UR
kb_checklists=
kb_reference=
description=The Anotonov-225 "MRIYA/DREAM". This one is the biggest and heaviest aircraft flying on Earth. She was designed to carry the Soviet space shuttle "Buran/Snowstorm". After spending years of inactivity at Kiev Airport after the Buran program was canceled, she was put back into service in 2001 to assist her smaller sister an124. This paint scheme shows her colours when carrying Buran.
ui_manufacturer=Antonov
ui_type=AN225
ui_variation=Antonov
ui_typerole=Heavy Freighter
ui_createdby=Tom
atc_heavy=1
atc_id=82005
atc_airline=ANTONOV
atc_parking_types=CARGO,MIL_CARGO,RAMP 
atc_flight_number=8266

[General]
atc_type=ANTONOV
atc_model=A225
editable=1
performance=6 LotarevD-18T with 229.5kN each. MTOW: over 600 metrical tons. MaxPayload over 250 metrical tons. Cruise speed:870km/h. Max Mach 0.77. Max payload range:4500km. Max fuel range:  15400km. Max ceiling: 12000 meters
Category=airplane

[CameraDefinition.0]
Title=Right Wingview
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Starboard wing as seen from the Flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=1.71, 2.79, 18.21
InitialPbh=2, 0, 150
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Left Wingview
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Port wing as seen from the Flightdeck
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=-1.71, 2.79, 18.21
InitialPbh=2, 0, 220
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Tail Camera
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Whole 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=.3
ShowWeather=Yes
InitialXyz=0, 15.06, -38.32
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Belly Camera
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Main gear from the bottom of the aircraft
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, -5.39, -11.67
InitialPbh=0, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Nose Gear Camera
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Camera attached to the portside nosegear
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=-0.94, -5.32, 15.89
InitialPbh=0, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title=Cargodeck Surveillance Front
Guid={15501D82-C0F9-40bd-9335-BED496704AB7}
Description=Surveillance camera on the cargodeck roof. Pointing to the nose
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=0, -0.29, 13.75
InitialPbh=2, 0, 180
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.6]
Title=Cargodeck Surveillance Rear
Guid={DF40A5DF-A129-4117-8075-9F4FA6DBFE2C}
Description=Surveillance camera on the cargodeck roof. Pointing to the stern
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=0, 0.83, -23-23
InitialPbh=2, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
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=.75
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.2, 0.0, 0.0
InitialPbh=0, 0, 0

[CameraDefinition.002]
Title=Radio Operator
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=0.3
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.20, 0, -1.85
InitialPbh=0, 0, 270

[CameraDefinition.003]
Title=Navigator
Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=0.3
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.20, 0, -1.10
InitialPbh=-0, 0, 270

[CameraDefinition.004]
Title=Engineer
Guid={4479D678-F256-4302-9BF7-D90C10D17165}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=0.3
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.05, 0, -1.10
InitialPbh=0, 0, 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 = 1322275                       // (pounds)
empty_weight = 385800                           // (pounds)

reference_datum_position     =  0, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -23, 0, 0     // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170.0,	  59.7,	 2.0,	 8.5     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170.0,	  59.7,	-2.0,	 8.5     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=700.0,	  50.9,	 0.0,	 8.5     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=1540.0,	  36.7,	 0.0,	 8.5     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=2140.0,	 -43.0,	 0.0,	 8.5     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=10000.0,	  30.0,	 0.0,	-2.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=10000.0,	   0.0,	 0.0,	-2.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=10000.0,	 -30.0,	 0.0,	-2.0     //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Pilot
station_name.1=Co-Pilot
station_name.2=Cockpitcrew
station_name.3=Upper Crewdeck
station_name.4=Upper Paxdeck
station_name.5=Cargo Front
station_name.6=Cargo Center
station_name.7=Cargo Rear

;Moments of Inertia
empty_weight_roll_MOI=13352310
empty_weight_pitch_MOI=24223159
empty_weight_yaw_MOI=39531785
empty_weight_coupled_MOI=0
CG_forward_limit = 0.000
CG_aft_limit = 1.000

[fuel]
LeftMain  =   -23.0, -28.0, 4.0, 38937.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
RightMain =   -23.0,  28.0, 4.0, 38937.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
LeftAux   =   -23.0, -36.5, 3.0,  6784.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
RightAux  =   -23.0,  36.5, 3.0,  6784.0, 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=9189.0                //Square feet
wing_span=290                 //Feet
wing_root_chord=58.8                  //Feet
wing_dihedral=-1.0                   //Degrees
wing_incidence=2.0                   //Degrees
wing_twist=-1.0                  //Degrees
oswald_efficiency_factor=0.81                  //Measure of lift effeciency of wing
wing_winglets_flag=0                     //Are winglets available?
wing_sweep=29.0                  //Degrees, wing leading edge
wing_pos_apex_lon=20.5                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=10                     //Feet, vertical distance from reference point, positive going up
htail_area=2470                  //Square feet
htail_span=72.8                  //Feet
htail_pos_lon=-121.4                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=10.0                   //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=1660                  //Square feet
vtail_span=37.1                  //Feet, tip to body
vtail_sweep=45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-120.5                //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=527                   //Square feet
aileron_area=325                   //Square feet
rudder_area=330                   //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=130.0                 //Knots True (KTAS)
full_flaps_stall_speed=102.0                 //Knots True (KTAS)
cruise_speed=475.0                 //Knots True (KTAS)
max_mach=0.77
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   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 5                                   // degrees
flaps-position.2 = 10                                   // degrees
flaps-position.3 = 15                                   // degrees
flaps-position.4 = 25                                   // degrees
flaps-position.5 = 35                                   // 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    = 0.3                                  // 0.0 .. 1.0
extending-time   = 15                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 6                                   // degrees
flaps-position.2 = 12                                   // degrees
flaps-position.3 = 18                                   // degrees
flaps-position.4 = 24                                   // degrees
flaps-position.5 = 30                                   // 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=0.7
rudder_effectiveness=0.7
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0	
aileron_trim_effectiveness=0.7
rudder_trim_effectiveness=0.7

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.6, -33.2, -3.9                 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -17.5, -58.6, -6.5                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -17.5, 58.6, -6.5                   //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -2.6, 33.2, -3.9                  //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.17                   //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=70.0                  //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                 //RPM, second stage compressor rated value
static_thrust=62866                 //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=1000.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=95
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,  63.0,    0.0, -20.2, 1000.0, 0, 3.0, 70.0, 1.4, 1.0, 0.900, 12.0,  12.0, 0, 200, 230
point.1 = 1, -47.2,   -13.5, -20.5, 3000.0, 1, 3.5, 13.0, 0.8, 2.0, 0.900, 15.0,  15.0, 2, 200, 230
point.2 = 1, -47.2,    13.5, -20.5, 3000.0, 2, 3.5, 13.0, 0.8, 2.0, 0.900, 15.0,  15.0, 3, 200, 230
point.3 = 2,  95.65,    0.0,   -3.76,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.4 = 2,  -55.57,	0.0,	-16.48,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.5 = 2,  -169.04,	0.0,	2.59,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.6 = 2,  -66.45,	-146.44,  -6.68,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0	
point.7 = 2,  -66.45,	146.44,	-6.68,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.8 = 2,  -178.66,	-60.34,	10.67,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.9 = 2,  -178.66,	60.34,	10.67,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.10 = 2,  -174.69,	0.0, 	39.05,  100.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
                      
static_pitch=-1.5
static_cg_height=18.6
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 = 70.57, -1.97, 9.0              ; 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,6taxi,7reco,8wing,9logo,10cabin                   
light.1 = 4,   69.65,    0.00,    9.68, fx_an124vc,
//light.2 = 9, -119.02,    8.79,   26.81, fx_an124tail,
//light.3 = 9, -119.02,   -8.79,   26.81, fx_an124tail,
light.2 = 1,   31.55,    0.00,   12.92, fx_an124beacon,
light.3 = 1,   16.12,    0.00,  -15.61, fx_an124beacon,
light.4 = 5,    -14.03,   70.87,   -6.72, fx_an124land,
light.5 = 5,    -14.03,  -70.87,   -6.72, fx_an124land,
light.6 = 5,   86.40,    0.00,  -17.25, fx_an124land,



[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
contrail=fx_contrail_l

[exits]
number_of_exits=4
exit.0=0.4,   58.10,  -12.50,  -6.79,  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,   2 //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)
exit.3=0.4, -60.58,   12.50,    -6.79, 1 //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

[smokesystem]
smoke.0 =  -31.9, -84.3,  -8.3, fx_engsmoke
smoke.1 =  -31.9, 84.3,  -8.3, fx_engsmoke
smoke.2 = -2.6, -33.2, -3.9, fx_engsmoke                 //(feet) longitudinal, lateral, vertical distance from reference datum
smoke.3 = -17.5, -58.6, -6.5, fx_engsmoke                  //(feet) longitudinal, lateral, vertical distance from reference datum
smoke.4 = -17.5, 58.6, -6.5, fx_engsmoke                   //(feet) longitudinal, lateral, vertical distance from reference datum
smoke.5 = -2.6, 33.2, -3.9, fx_engsmoke                  //(feet) longitudinal, lateral, vertical distance from reference datum