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Topic: Can Someone Please Post The Aircraft.cfg (Learjet)
Username: B737-112
Posted 2009-09-27 17:19:56 and read 7177 times.

I need the default Learjet 45 aircraft.cfg info, if you would be kind enough to copy and paste it here.

Thanks so much,
Ryan

Topic: RE: Can Someone Please Post The Aircraft.cfg (Learjet)
Username: Dalb777
Posted 2009-09-27 20:24:26 and read 7162 times.

I'm assuming for FS 2004???

[fltsim.0]
title=Learjet 45
sim=Lear45
model=
panel=
sound=
texture=
kb_checklists=Lear45_check
kb_reference=Lear45_ref
atc_id=N456LJ
ui_manufacturer=Bombardier
ui_type="Learjet 45"
ui_variation="White with gold and black"
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."
atc_parking_types=RAMP

[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"
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."
atc_parking_types=RAMP

[General]
atc_type=Learjet
atc_model=
editable=0
performance="Cruise SpeedtnMach 0.81 464 kts 859 kmhnnEnginestnAllied Signal TFE731-20 3,500 lb thrustnnMaximum Rangetn2,200 nm 2,532 sm t 4,074 kmnnService Ceilingtn51,000 ft 15,545 mnnFuel Capacitytn6,062 lb 2,722 kgn905 U.S. gal 3,424 L nnMaximum Gross Weighttn20,450 lb 9,276 kgnnMaximum Takeoff Weight - HGWtn20,200 lb t9,163 kgnnUseful Loadtn8,750 lb t3,969 kgnnLengthtn58.4 ftt 17.7 mnnWingspantn47.8 ftt 14.6 mnnHeighttn14.3 ftt 4.3 mnnSeatingtnUp to 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, Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -17.0, 1.2, 0.0, Co-Pilot" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, -22.5, -1.2, 0.0, Passenger 1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, -22.5, 1.2, 0.0, Passenger 2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "170, -26.7, -1.2, 0.0, Passenger 3" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "170, -26.7, 1.2, 0.0, Passenger 4" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "0, -30.9, -1.2, 0.0, Passenger 5" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "0, -30.9, 1.2, 0.0, Passenger 6" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0, -35.1, -1.2, 0.0, Passenger 7" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0, -35.1, 1.2, 0.0, Passenger 8" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "100, -42.0, 0.0, 0.0, Baggage1" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "50, -45.0, 0.0, 0.0, Baggage2" // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)


;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 = 12.0
generator_alternator_voltage = 13.8
max_generator_alternator_amps = 40.0

;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0

[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?

[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

[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

[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, -1.435, 3.012

[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, -16.00, 0.00, 2.25, fx_vclight,
light.9 = 4, -27.00, 0.00, 0.25, fx_vclighth,

[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, 0
Com.2 = 1, 0
Nav.1 = 1, 0, 1
Nav.2 = 1, 0, 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 = 1

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

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

[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=25.0
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

Topic: RE: Can Someone Please Post The Aircraft.cfg (Learjet)
Username: B737-112
Posted 2009-09-27 21:36:46 and read 7154 times.

It's actually FSX, I forgot to mention that. I assume this will work, I'll give it a try.

Thank you.


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