Jesperi Lauhio

Wilco A343 + Thomas Ruth Merge

2 viestiä aiheessa

Tossa oma cfg ja siis wilcon paneelilla. Siitä vaan vertailemaan  ;D

Koneena siis Thomaksen A340-300

 

[fltsim.0]

title=Feelthere A340-300 GULF

sim=FeelThere_A340-300

model=

panel=

sound=

texture=GA

kb_checklists=

kb_reference=

atc_id=AB-TOM

atc_airline=Gulf Air

atc_flight_number=1123

atc_heavy=1

ui_manufacturer="Airbus"

ui_type="A340-300"

ui_variation="Gulf Air"

ui_typerole="Commercial Airliner"

ui_createdby=

description=

 

[fltsim.1]

title=Finnair A340-313E NC

sim=FeelThere_A340-300

model=

panel=

sound=

texture=FIN_NC

kb_checklists=

kb_reference=

atc_id=OH-LQC

atc_airline=Finnair

atc_flight_number=62

atc_heavy=1

ui_manufacturer="Airbus"

ui_type="A340-300"

ui_variation="Finnair NC"

ui_typerole="Commercial Airliner"

ui_createdby=

description=One of the last widebodies of Finnair to be repainted into the new color scheme despite being one of the oldest widebodies in the fleet.

 

[fltsim.2]

title=Finnair Unikko-livery Airbus A340-300

sim=FeelThere_A340-300

model=

panel=

sound=

texture=unikko

kb_checklists=

kb_reference=

atc_id=OH-LQD

atc_airline=Finnair

atc_flight_number=1123

atc_heavy=1

ui_manufacturer="Airbus"

ui_type="A340-300"

ui_variation="Finnair unikko"

ui_typerole="Commercial Airliner"

ui_createdby=

description=

 

[General]

atc_type=AIRBUS

atc_model=A343

editable=1

performance="Reisegeschwindigkeit\nMach 0.84         555 mph         893 kmh\n\nTriebwerkoption        \nP&W 4000\nRR Trent 800\nGE 90 series\n\nMaximale Reichweite              \n5.960 nm          6.859 sm        11.038 km\n\nDienstgipfelhöhe    \n42.000 Fuß           12.800 m\n\nTreibstoffmenge       \n45.220 Gallonen        171.160 L \n\nMaximales Startgewicht     \n660.000 lbs        299.370 kg\n\nLänge    \n242 Fuß, 4 Zoll         73.9 m\n\nSpannweite      \n199 Fuß, 11 Zoll          60.9 m\n\nHöhe        \n60 Fuß, 8 Zoll           18.5 m\n\nSitzplätze       \n386 bis 550 \n\nFrachtkapazität        \n7.552 Kubikfuß              213.8 Kubikmeter\n"

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, 1.183, -9.753

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, 1.183, -9.753

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=-1.914, 1.046, 26.133

InitialPbh=5, 0, 215

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=1.914, 1.046, 26.133

InitialPbh=5, 0, 145

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, -3.127, -19.004

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, -4.33, 26.056

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, 12.155, -33.902

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=Jump Seat

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, 0.00, -1.2

InitialPbh=2, 0, 0

 

[WEIGHT_AND_BALANCE]

reference_datum_position=0.00000,0.000000,0.000000

max_number_of_stations=50

 

station_load.0 =   "950,    42.0, 0.0, 0.0, Crew"

station_load.1 =   "5000,  37.0, 0.0, 0.0, Galleys"

station_load.2 ="36285,   16.0, 0.0, 0.0, Baggage"

station_load.3 ="36298,   0.0, 0.0, 0.0, Cargo"       

station_load.4 ="2480,   26.0, 0.0, 0.0, First"

station_load.5 ="34556,  0.0, 0.0, 0.0, Coach"

 

empty_weight=287000

max_gross_weight=610000

empty_weight_roll_MOI=33200000

empty_weight_pitch_MOI=34400000

empty_weight_yaw_MOI=22800000

empty_weight_coupled_MOI=0.0

empty_weight_CG_position=0.000,  0.000,  0.000

 

 

[flight_tuning]

cruise_lift_scalar=1.0

parasite_drag_scalar=1.0

induced_drag_scalar=1.1

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=0.8

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 = -18.09, -64.14, -4.67                    //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1 = 3.28, -30.96, -8.59                    //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.2 = 3.28,  30.96, -8.59                    //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.3 = -18.09,  64.14, -4.67                    //(feet) longitudinal, lateral, vertical distance from reference datum

//fuel_flow_scalar = 1.0      ORIGINAL

fuel_flow_scalar = 0.8217                     //Scalar for fuel flow efficiency

min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

max_contrail_temperature=-30       

 

[TurbineEngineData]

fuel_flow_gain = 0.002                          //Gain on fuel flow

inlet_area = 28.9                              //Square Feet, engine nacelle inlet area

rated_N2_rpm = 29920                            //RPM, second stage compressor rated value

static_thrust = 34000                          //Lbs, max rated static thrust at Sea Level

afterburner_available = 0                       //Afterburner available?

reverser_available = 1                          //Thrust reverser available?

 

[jet_engine]

thrust_scalar = 1.0

 

[electrical]

max_battery_voltage = 24

generator_alternator_voltage = 28

max_generator_alternator_amps = 200

electric_always_available =0

flap_motor         =3, 0 , 17.0

gear_motor         =3, 0 , 17.0

autopilot          =3, 0 , 17.0

avionics_bus       =3, 0 , 17.0

avionics           =1, 0 , 17.0

pitot_heat         =3, 0 , 17.0

additional_system  =3, 0 , 17.0

marker_beacon      =3, 0 , 17.0

gear_warning       =3, 0 , 17.0

fuel_pump          =3, 0 , 17.0

starter1           =3, 0 , 17.0

starter2           =3, 0 , 17.0

light_nav          =3, 0 , 17.0

light_beacon       =3, 0 , 17.0

light_landing      =3, 0 , 17.0

light_taxi         =3, 0 , 17.0

light_strobe       =3, 0 , 17.0

light_panel        =3, 0 , 17.0

light_cabin        =3, 0 , 17.0

auto_brakes        =3, 0 , 17.0

standby_vacuum     =3, 0 , 17.0

hydraulic_pump     =3, 0 , 17.0

fuel_transfer_pump =3, 0 , 17.0

light_recognition  =3, 0 , 17.0

light_wing         =3, 0 , 17.0

light_logo         =3, 0 , 17.0

directional_gyro   =3, 0 , 17.0

directional_gyro_slaving =3, 0 , 17.0

 

 

        //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)

 

[contact_points]

point.0=1,  66.95,   0.00, -16.43, 1181.1, 0, 4.521, 90.0, 1.00, 2.5, 0.7235, 4.0, 4.0, 0, 270.0, 270.0

point.1=1, -18.60, -17.60, -18.38, 1574.8, 1, 4.521,  0.0, 2.61, 1.6, 0.7470, 6.9, 6.9, 2, 270.0, 270.0

point.2=1, -18.60,  17.60, -18.38, 1574.8, 2, 4.521,  0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0

point.3=1, -18.60,   0.05, -18.38, 1574.8, 2, 4.521,  0.0, 2.61, 1.6, 0.7470, 7.1, 7.1, 3, 270.0, 270.0

point.4=2, -43.97, -97.21,   4.80,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0

point.5=2, -43.97,  97.21,   4.80,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0

point.6=2, -107.2,   0.00,   2.53,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0

point.7=2,  86.35,   0.00,   0.00,  787.4, 0, 0.000,  0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0

 

static_pitch = 0.10

static_cg_height = 17.56

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 = 0.86  //Brake scalar

auto_brakes=4

 

[hydraulic_system]

normal_pressure = 3000.0    //PSI

electric_pumps  = 1         //no electric pumps

engine_map      = 1,1,1,1   //pumps on Eng1,2

 

[Views]

//eyepoint = 69.66, -1.43, 3.65

eyepoint = 79.854, -1.76, 3.60

 

[Flaps.0]

type=1

span-outboard=0.500000

extending-time=20.000000

system_type=1

flaps-position.0=0.000000,0.000000

flaps-position.1=0.0

flaps-position.2=15.0 //nominal value should be10 but we need big effect RY

flaps-position.3=20.0 //ditto to accomodate flap 2

flaps-position.4=26.0 //ditto to accomodate flap 2

flaps-position.5=35.0 //ditto to accomodate flap 2

 

 

[Flaps.1]

type=2

span-outboard=0.800

extending-time=20.000

system_type=1

damaging-speed=232.000

blowout-speed=250.000

lift_scalar=0.3

drag_scalar=0.7

pitch_scalar=0.0

flaps-position.0=0

flaps-position.1=18.0

flaps-position.2=18.0

flaps-position.3=22.0

flaps-position.4=22.0

flaps-position.5=27.0

 

[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

Adf.2=1

Transponder.1=1

Marker.1=1

 

[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

 

[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

direction_indicator.1=3,0

 

[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]

max_pressure=5.15   // PSI

vacuum_type=2       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

 

[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

 

[pneumatic_system]

max_pressure=18.000000

bleed_air_scalar=1.000000

 

[LIGHTS]       

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing,6taxi,7reco,8wing,9logo,10cabin

light.0 = 1, -22.38,   0.00, -10.70, fx_T332beacon ,

light.1 = 1,  17.22,   0.00,   9.74, fx_T332beacon ,

light.2 = 2,-118.31,   0.00,   6.60, fx_strobeh ,

light.3 = 3,-118.31,   0.00,   6.60, fx_navwhih ,

light.4 = 5,  26.04,  18.39,  -3.28, fx_T332land  ,

light.5 = 5,  26.04, -18.39,  -3.28, fx_T332land  ,

light.6 = 3,-103.26,   8.79,  20.02, fx_T332logo  ,

light.7 = 3,-103.26,  -8.79,  20.02, fx_T332logo  ,

light.8 = 4,  79.14,   0.00,   4.56, fx_vclighth  ,

//light.9 = 6,  22.64,  29.49,  -8.18, fx_T332eng  ,

//light.10 = 6,  22.64, -29.49,  -8.18, fx_T332eng  ,

//light.11 = 8, -15.35,  66.26,   2.70, fx_T332wing  ,

//light.12 = 8, -15.35, -66.26,   2.70, fx_T332wing  ,

 

 

[EFFECTS]

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn, 1

 

[exits]

number_of_exits = 4

exit.0 = 0.4,  68.87, -6.0, 6.5, 0    ;Percent per second

exit.1 = 0.04,   -66.35,  7.497, -4.905, 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

 

 

[fuel]

Center1   =  -10.5,   0.0, -8.2, 11188.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

Center2   =  -100.5,   0.0, 5.7, 1646.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftMain  = -8.9, -27.9,  -1.7,  11247.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightMain = -8.9,  27.9,  -1.7,  11247.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftAux  = -36.3, -67.9,  2.5,  964.0, 3.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightAux = -36.3,  67.9,  2.5,  964.0, 3.0     //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               = 3893.0                //Square feet

wing_span               = 197.83                 //Feet

wing_root_chord         = 35.1                  //Feet

wing_dihedral           = 5.5                   //Degrees

wing_incidence          = 1.0                   //Degrees

wing_twist              = -0.5                  //Degrees

oswald_efficiency_factor= 0.72                   //Measure of lift effeciency of wing

wing_winglets_flag      = 1                     //Are winglets available?

wing_sweep              = 31.5                  //Degrees, wing leading edge

wing_pos_apex_lon       = 20.0                  //Feet, longitudinal distance from reference point, negative going aft

wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up

htail_area              = 716.9                //Square feet

htail_span              = 63.16                  //Feet

htail_pos_lon           = -100.07                //Feet, longitudinal distance from reference point, negative going aft

htail_pos_vert          = 5.87                   //Feet, vertical distance from reference point, positive going up

htail_incidence         = 0.0                   //Degrees

htail_sweep             = 34.0                  //Degrees, horizontal tail leading edge

vtail_area              = 583.0                 //Square feet

vtail_span              = 30.84                  //Feet, tip to body

vtail_sweep             = 39.0                  //Degrees, vertical tail leading edge

vtail_pos_lon           = -99.74                //Feet, longitudinal distance from reference point, negative going aft

vtail_pos_vert          = 25.6                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 85.9                 //Square feet

aileron_area            = 48.0                  //Square feet

rudder_area             = 121.0                 //Square feet

elevator_up_limit       = 30.0                  //Degrees

elevator_down_limit     = 15.0                  //Degrees

aileron_up_limit        = 30.0                  //Degrees

aileron_down_limit      = 15.0                  //Degrees

rudder_limit            = 25.0                  //Degrees

elevator_trim_limit     = 15.0                  //Degrees

spoiler_limit           = 60.0                  //Degrees

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

spoiler_extension_time=2.000000

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

//fly_by_wire=1

 

[Reference Speeds]

flaps_up_stall_speed    = 150.0                 //Knots True (KTAS)

full_flaps_stall_speed  = 120.0                 //Knots True (KTAS)

cruise_speed            = 482.0                 //Knots True (KTAS)

max_mach                = 0.86

max_indicated_speed     = 340                   //Red line (KIAS)

 

[autopilot]

autopilot_available=1

flight_director_available=1

default_vertical_speed=1800.000000

autothrottle_available=1

autothrottle_arming_required=1

autothrottle_takeoff_ga=1

autothrottle_max_rpm=90.000000

pitch_takeoff_ga=8.000000

max_pitch=10.000000

max_pitch_acceleration=0.8

max_pitch_velocity_lo_alt=1.0

max_pitch_velocity_hi_alt=1.0

max_pitch_velocity_lo_alt_breakpoint=20000.000000

max_pitch_velocity_hi_alt_breakpoint=28000.000000

max_bank=25.0,15.0

max_bank_acceleration=3.0

max_bank_velocity=3.000000

max_throttle_rate=0.100000

nav_proportional_control=9.000000

nav_integrator_control=0.250000

nav_derivative_control=0.000000

nav_integrator_boundary=2.500000

nav_derivative_boundary=0.000000

gs_proportional_control=9.520000

gs_integrator_control=0.260000

gs_derivative_control=0.000000

gs_integrator_boundary=0.700000

gs_derivative_boundary=0.000000

yaw_damper_gain=0.000000

 

 

[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

 

[TailHook]

tailhook_length=4                               ;(feet)

tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum

cable_force_adjust=0.9

 

// Added to inhibit the FSX built-in GPWS

[GPWS]

max_warning_height         =  0

sink_rate_fpm              = -99999

excessive_sink_rate_fpm    = -99999

climbout_sink_rate_fpm     = -99999

flap_and_gear_sink_rate_fpm= -99999

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