Request aircraft.cfg file for Lear45

[BobKK47 2]

I inadvertently deleted the aircraft.cfg file for the stock Lear45.  Could someone post it here or send it to my AVSIM mailbox?

 

Thank you.

[JSkorna 137]

[fltsim.0]

title=Learjet 45

sim=Lear45

model=

panel=

sound=

texture=

kb_checklists=Lear45_check

kb_reference=Lear45_ref

atc_id=JA-068X

ui_manufacturer="Bombardier"

ui_type="Learjet 45"

ui_variation="Gold, Black"

ui_typerole="Twin Engine Jet"

ui_createdby="Microsoft Corporation"

description="The Model 45 is Learjet's first all-new aircraft since Bill Lear's first Model 23. Although it looks like a Learjet, it has only half the parts of a Model 35, reflecting a significant design progression. The parameters set down for the 45 called for it to have the performance of the Learjet 35, the handling of the Learjet 31A, and greater cabin space than the competition."

 

[fltsim.1]

title=Learjet 45 Limited Edition

sim=Lear45

model=

panel=

sound=

texture=1

kb_checklists=Lear45_check

kb_reference=Lear45_ref

atc_id=N45LR

ui_manufacturer="Bombardier"

ui_type="Learjet 45"

ui_variation="Anniversary edition"

ui_typerole="Twin Engine Jet"

ui_createdby="Microsoft Corporation"

description="The Model 45 is Learjet's first all-new aircraft since Bill Lear's first Model 23. Although it looks like a Learjet, it has only half the parts of a Model 35, reflecting a significant design progression. The parameters set down for the 45 called for it to have the performance of the Learjet 35, the handling of the Learjet 31A, and greater cabin space than the competition."

 

[General]

atc_type=BOMBARDIER

atc_model=LJ45

editable=0

performance="Cruise Speed\t\nMach 0.81            464 kts          859 kmh\n\nEngines\t\nAllied Signal TFE731-20     3,500 lb thrust\n\nMaximum Range\t\n2,200 nm            2,532 sm \t     4,074 km\n\nService Ceiling\t\n51,000 ft             15,545 m\n\nFuel Capacity\t\n6,062 lb              2,722 kg\n905 U.S. gal         3,424 L \n\nMaximum Gross Weight\t\n20,450 lb             9,276 kg\n\nMaximum Takeoff Weight - HGW\t\n20,200 lb \t9,163 kg\n\nUseful Load\t\n8,750 lb  \t3,969 kg\n\nLength\t\n58.4 ft\t               17.7 m\n\nWingspan\t\n47.8 ft\t               14.6 m\n\nHeight\t\n14.3 ft\t               4.3 m\n\nSeating\t\nUp to 9"

Category = airplane

 

[CameraDefinition.0]

Title = "Tail"

Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}

Description = Looking forward from behind the aircraft

Origin = Center

SnapPbhAdjust = Swivel

SnapPbhReturn = FALSE

PanPbhAdjust = Swivel

PanPbhReturn = FALSE

Track = None

ShowAxis = FALSE

AllowZoom = TRUE

InitialZoom = .75

ShowWeather = Yes

InitialXyz = 0, 2.3, -20.0

InitialPbh = 10, 0, 0

XyzAdjust = TRUE

Category=Aircraft

MomentumEffect=TRUE

ClipMode=Minimum

 

[CameraDefinition.1]

Title = "Right Wing"

Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}

Description = View from the right wing tip looking at the cockpit

Origin = Center

SnapPbhAdjust = Swivel

SnapPbhReturn = FALSE

PanPbhAdjust = Swivel

PanPbhReturn = FALSE

Track = None

ShowAxis = FALSE

AllowZoom = TRUE

InitialZoom = 0.5

ShowWeather = Yes

InitialXyz = 10.8, 1.4, -2.0

InitialPbh = 6, 0, 290

XyzAdjust = TRUE

Category=Aircraft

MomentumEffect = FALSE

ClipMode=Minimum

 

[CameraDefinition.2]

Title = "Left Wing"

Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}

Description = View from the left wing tip looking at the cockpit

Origin = Center

SnapPbhAdjust = Swivel

SnapPbhReturn = FALSE

PanPbhAdjust = Swivel

PanPbhReturn = FALSE

Track = None

ShowAxis = FALSE

AllowZoom = TRUE

InitialZoom = 0.5

ShowWeather = Yes

InitialXyz = -10.8, 1.4, -2.0

InitialPbh = 6, 0, 70

XyzAdjust = TRUE

Category=Aircraft

MomentumEffect = No

ClipMode=Minimum

 

[CameraDefinition.001]

Title = "Radio Stack"

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 = 1.5

SmoothZoomTime = 2.0

ZoomPanScalar = 1.0

ShowWeather = Yes

XyzAdjust = TRUE

ShowLensFlare=FALSE

Category = Cockpit

PitchPanRate=20

HeadingPanRate=60

InitialXyz=0.45, -0.25, -0.1

InitialPbh=14.2, 0, 0

 

[CameraDefinition.002]

Title = "Engine Controls"

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 = 1.1

SmoothZoomTime = 2.0

ZoomPanScalar = 1.0

ShowWeather = Yes

XyzAdjust = TRUE

ShowLensFlare=FALSE

Category = Cockpit

PitchPanRate=20

HeadingPanRate=60

InitialXyz=0.30, 0.09, -0.18

InitialPbh=48.5, 0, 9

 

[WEIGHT_AND_BALANCE]

max_gross_weight = 20450.0                      // (pounds)

empty_weight = 11700.0                          // (pounds)

 

reference_datum_position     =   34.5,  0, 0    // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)

empty_weight_CG_position     =  -35.79, 0, 0    // (feet) longitudinal, lateral, vertical distance from specified datum

 

max_number_of_stations = 50

 

station_load.0  = 170, -17.0, -1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.1  = 170, -17.0,  1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.2  = 170, -22.5, -1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.3  = 170, -22.5,  1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.4  = 170, -26.7, -1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.5  = 170, -26.7,  1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.6  = 0,   -30.9, -1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.7  = 0,   -30.9,  1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.8  = 0,   -35.1, -1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.9  = 0,   -35.1,  1.2, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.10 = 100, -42.0,  0.0, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.11 =  50, -45.0,  0.0, 0.0     // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)

 

station_name.0  = "Pilot"       

station_name.1  = "Co-Pilot"    

station_name.2  = "Passenger 1" 

station_name.3  = "Passenger 2" 

station_name.4  = "Passenger 3" 

station_name.5  = "Passenger 4" 

station_name.6  = "Passenger 5" 

station_name.7  = "Passenger 6" 

station_name.8  = "Passenger 7" 

station_name.9  = "Passenger 8" 

station_name.10 = "Baggage1"    

station_name.11 = "Baggage2"           

 

;Moments of Inertia

empty_weight_pitch_MOI   = 50000

empty_weight_roll_MOI    = 45000

empty_weight_yaw_MOI     = 70000

empty_weight_coupled_MOI = 0.0

 

[electrical]

max_battery_voltage = 24.0

generator_alternator_voltage = 28.0

max_generator_alternator_amps = 400.0

 

[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 = -42.8, -4.8, 0.8                     //(feet) longitudinal, lateral, vertical distance from reference datum

Engine.1 = -42.8,  4.8, 0.8                     //(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          = 0.0025                //Gain on fuel flow

inlet_area              = 4.2895                //Square Feet, engine nacelle inlet area

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

static_thrust           = 3500                  //Lbs, max rated static thrust at Sea Level

afterburner_available   = 0                     //Afterburner available?

reverser_available      = 1                     //Thrust reverser available?

ThrustSpecificFuelConsumption = 0.5             //Thrust specific fuel consumption (Jets)

AfterBurnThrustSpecificFuelConsumption = 0      //TSFC with afterburn/reheat engaged 

 

[jet_engine]

thrust_scalar = 1.0

 

 

        //0  Class

        //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

[contact_points]

point.0=1, -10.00,   0.00, -4.35, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.5, 0.9100, 10.0, 10.0, 0, 260.0, 260.0

point.1=1, -37.25,  -4.75, -4.87, 1574.8, 1, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  9.0,  9.0, 2, 260.0, 260.0

point.2=1, -37.25,   4.75, -4.87, 1574.8, 2, 0.6349,  0.0, 0.4798, 2.5, 0.5456,  9.0,  9.0, 3, 260.0, 260.0

point.3=2, -37.83, -23.92, -3.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0

point.4=2, -37.83,  23.92, -3.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0

point.5=2, -57.17,   0.00,  0.00,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0

point.6=2, -11.47,   0.00, -1.50,  787.4, 0, 0.0000,  0.0, 0.0000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

 

static_pitch = -0.84

static_cg_height = 4.36

gear_system_type=1           //Hydraulic

emergency_extension_type=2   //None=0,Pump=1,Gravity=2

 

[gear_warning_system]

gear_warning_available = 1    //Normal

pct_throttle_limit =  0.1     //Percent throttle that activates warning

flap_limit_idle    = 15.0     //Flap angle that activates warning at idle

flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

 

[brakes]

parking_brake = 1       //Parking brake available

toe_brakes_scale = 1.2  //Brake scalar

auto_brakes = 0

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      = 1,1,0,0   //pumps on Eng1,2

 

[Views]

eyepoint = -16.385, -1.3, 3.15

 

[LIGHTS]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  -39.00, -23.6,  -0.25, fx_navredm ,

light.1 = 3,  -39.00,  23.6,  -0.25, fx_navgrem ,

light.2 = 3,  -63.63,   0.00,  9.20, fx_navwhi ,

light.3 = 1,  -37.00,   0.00, -2.59, fx_beaconb ,

light.4 = 2,  -36.97,   0.00, -2.62, fx_strobe ,

light.5 = 1,  -63.05,   0.00,  9.75, fx_beaconh ,

//light.6 = 5,  -29.7,   -1.3,  -1.71, fx_landing ,

//light.7 = 5,  -29.7,    1.3,  -1.71, fx_landing ,

//light.8 = 4,  -26.00,   0.00,  2.00, fx_vclighth,

//light.9 = 4,  -14.00,   0.00,  1.90, fx_vclight,

 

[flaps.0]

type             = 1                                    // 1 - tail, 2 - lead

span-outboard    = 0.8                                  // 0.0 .. 1.0

extending-time   = 5                                    // seconds

flaps-position.0 = 0                                    // degrees

flaps-position.1 = 8                                    // degrees

flaps-position.2 = 20                                   // degrees

flaps-position.3 = 40                                   // degrees

damaging-speed   = 250                                  // KIAS

blowout-speed    = 300                                  // KIAS

 

[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

 

[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

 

[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

 

[airspeed_indicators]

airspeed_indicator.0=1

airspeed_indicator.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

 

[pneumatic_system]

max_pressure=18.000000

bleed_air_scalar=1.000000

 

[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

 

[EFFECTS]

wake=fx_wake

water=fx_spray

dirt=fx_tchdrt

concrete=fx_sparks

touchdown=fx_tchdwn_s, 1

 

[fuel]

Center1   =  -41.4,   0.0, -1.5, 359.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

LeftMain  =  -36.3, -10.0, -1.5, 268.5, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

RightMain =  -36.3,  10.0, -1.5, 268.5, 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

 

[airplane_geometry]

wing_area               = 312.0                 //Square feet

wing_span               = 45.8                  //Feet

wing_root_chord         = 9.9                   //Feet

wing_dihedral           = 2.5                   //Degrees

wing_incidence          = 0.5                   //Degrees

wing_twist              = -1.5                  //Degrees

oswald_efficiency_factor= 0.8                   //Measure of lift effeciency of wing

wing_winglets_flag      = 1                     //Are winglets available?

wing_sweep              = 13.4                  //Degrees, wing leading edge

wing_pos_apex_lon       = -31.5                 //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              = 67.0                  //Square feet

htail_span              = 17.2                  //Feet

htail_pos_lon           = -59.1                 //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         = 2.0                   //Degrees

htail_sweep             = 25.0                  //Degrees, horizontal tail leading edge

vtail_area              = 42.0                  //Square feet

vtail_span              = 7.4                   //Feet, tip to body

vtail_sweep             = 30.0                  //Degrees, vertical tail leading edge

vtail_pos_lon           = -55.0                 //Feet, longitudinal distance from reference point, negative going aft

vtail_pos_vert          = 4.1                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 17.0                  //Square feet

aileron_area            = 13.5                  //Square feet

rudder_area             = 7.3                   //Square feet

elevator_up_limit       = 17.0                  //Degrees

elevator_down_limit     = 15.5                  //Degrees

aileron_up_limit        = 18.0                  //Degrees

aileron_down_limit      = 18.0                  //Degrees

rudder_limit            = 30.0                  //Degrees

elevator_trim_limit     = 15.0                  //Degrees

spoiler_limit           = 60.0                  //Degrees

spoiler_extension_time  = 2.0                   //Seconds

spoilerons_available    = 1                     //Spoilerons Available?

aileron_to_spoileron_gain = 4.6                 //Aileron to spoileron gain

min_ailerons_for_spoilerons = 5                 //Degrees

min_flaps_for_spoilerons= 0.0                   //Minimum flap handle position when spoilerons activate

auto_spoiler_available   = 1

positive_g_limit_flaps_up  =  3.0               //Design G load tolerance (positive, flaps up)

positive_g_limit_flaps_down=  2.0               //Design G load tolerance (positive, flaps down) 

negative_g_limit_flaps_up  = -2.0               //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    = 112.0                 //Knots True (KTAS)

full_flaps_stall_speed  = 102.0                 //Knots True (KTAS)

cruise_speed            = 464.0                 //Knots True (KTAS)

max_mach                = 0.81

max_indicated_speed     = 330                   //Red line (KIAS)

 

[autopilot]

autopilot_available= 1

flight_director_available= 1

default_vertical_speed= 1800.0

autothrottle_available= 1

autothrottle_arming_required= 0

autothrottle_max_rpm = 90

autothrottle_takeoff_ga= 0

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=27,14

max_bank_acceleration=1.8

max_bank_velocity=3.00

max_throttle_rate=0.10

nav_proportional_control=11.00

nav_integrator_control=0.20

nav_derivative_control=0.00

nav_integrator_boundary=2.50

nav_derivative_boundary=0.00

gs_proportional_control=9.52

gs_integrator_control=0.26

gs_derivative_control=0.00

gs_integrator_boundary=0.70

gs_derivative_boundary=0.00

yaw_damper_gain = 1.0

 

[forcefeedback]

stick_shaker_magnitude=5000             ; 0 - 10000

stick_shaker_direction=0                ; 0 - 35999 degrees

stick_shaker_period=111111              ; in microseconds

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=9000           ; 0 - 35999 degrees

gear_bump_left_duration=250000          ; in microseconds

gear_bump_right_magnitude=2700          ; 0 - 10000

gear_bump_right_direction=27000         ; 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

[BobKK47 2]

Thanks, Jim.