// Learjet60 ver 25 // Copyright PAD 2007 // Updated Jan 15, 2007 // FSX // [fltsim.0] title=Learjet60_C-FBCD sim=Lear60 model= panel= sound= texture=FBCD kb_checklists=Lear60_check kb_reference=FSX_Lear60_ref atc_id=C-FBCD ui_manufacturer=Bombardier ui_type="Learjet 60" ui_variation=Aviation CMP Inc ui_typerole="Twin Engine Jet" ui_createdby="Premier Aircraft Design" description=Bombardier Learjet 60 - Flightcrew of two. Optional seating arrangements for six to nine passengers. [fltsim.1] title=Learjet60_D-CWHS sim=Lear60 model= panel= sound= texture=CWHS kb_checklists=Lear60_check kb_reference=FSX_Lear60_ref atc_id=D-CWHS ui_manufacturer=Bombardier ui_type="Learjet 60" ui_variation=Cirrus Aviation ui_typerole="Twin Engine Jet" ui_createdby="Premier Aircraft Design" description=Bombardier Learjet 60 - Flightcrew of two. Optional seating arrangements for six to nine passengers. [fltsim.2] title=Learjet60_G-LGAR sim=Lear60 model= panel= sound= texture=LGAR kb_checklists=Lear60_check kb_reference=FSX_Lear60_ref atc_id=G-LGAR ui_manufacturer=Bombardier ui_type="Learjet 60" ui_variation=TAG Aviation ui_typerole="Twin Engine Jet" ui_createdby="Premier Aircraft Design" description=Bombardier Learjet 60 - Flightcrew of two. Optional seating arrangements for six to nine passengers. [fltsim.3] title=Learjet60_N232LJ sim=Lear60 model= panel= sound= texture=N232 kb_checklists=Lear60_check kb_reference=FSX_Lear60_ref atc_id=N232LJ ui_manufacturer=Bombardier ui_type="Learjet 60" ui_variation=Bombardier Aerospace ui_typerole="Twin Engine Jet" ui_createdby="Premier Aircraft Design" description=Bombardier Learjet 60 - Flightcrew of two. Optional seating arrangements for six to nine passengers. [fltsim.4] title=Learjet60_N838RC sim=Lear60 model= panel= sound= texture=N838 kb_checklists=Lear60_check kb_reference=FSX_Lear60_ref atc_id=N838RC ui_manufacturer=Bombardier ui_type="Learjet 60" ui_variation=RC Airways Inc ui_typerole="Twin Engine Jet" ui_createdby="Premier Aircraft Design" description=Bombardier Learjet 60 - Flightcrew of two. Optional seating arrangements for six to nine passengers. [General] atc_type=Learjet atc_model= performance=Max Cruise Speed\tMach .81\nMaximum Range\t2,450 nm\nService Ceiling\t51,000 ft\nMax Gross Weight\t23,500 lb\nSeating\t\tUp to 9\nUseful Load\t2,850 lb 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 [Views] eyepoint = -16.7, -1.6, 2.0 [WEIGHT_AND_BALANCE] max_gross_weight = 23500.0 // (pounds) empty_weight = 13850.0 // (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 = 0, -22.5, -1.2, 0.0, Passenger 1 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 0, -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 = 170, -30.9, -1.2, 0.0, Passenger 5 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = 170, -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 = 24.0 generator_alternator_voltage = 30.0 max_generator_alternator_amps = 400.0 ;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 = 1.1 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.1 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.2 //1.1 roll_stability = 1.15 //1.1 yaw_stability = 1.0 elevator_trim_effectiveness = 1.1 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 = -50.00, -4.3, 2.3 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -50.00, 4.3, 2.3 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.950 //Scalar for fuel flow efficiency min_throttle_limit = -0.40 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.0025 //Gain on fuel flow inlet_area = 4.00000 //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 = 1.00 //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, -11.70, 0.00, -5.25, 1574.8, 0, 0.800, 30.0, 0.1700, 5.5, 0.9100, 5.0, 4.0, 0, 260.0, 260.0 point.1=1, -37.50, -4.75, -5.49, 1574.8, 1, 0.800, 0.0, 0.4798, 2.5, 0.5456, 6.0, 5.0, 2, 260.0, 260.0 point.2=1, -37.50, 4.75, -5.49, 1574.8, 2, 0.800, 0.0, 0.4798, 2.5, 0.5456, 6.0, 5.0, 3, 260.0, 260.0 point.3=2, -43.00, -21.00, 2.00, 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, -43.00, 21.00, 2.00, 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, -62.00, 0.00, 2.00, 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, -5.00, 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 point.7=5, -5.00, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch = 0.00 static_cg_height = 5.50 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 = 0.65 //Brake scalar //1.2 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -38.50, -19.0, -1.2, fx_navredm , light.1 = 3, -38.50, 19.0, -1.2, fx_navgrem , light.2 = 3, -61.90, 0.00, 2.40, fx_navwhi , light.3 = 1, -33.70, 0.00, -2.99, fx_PADbeaconh , light.4 = 1, -59.7, 0.00, 9.60, fx_PADbeaconh , light.5 = 2, -61.90, 0.00, 2.40, fx_strobe , light.6 = 2, -59.7, 0.00, 9.60, fx_strobe , light.7 = 4, -16.00, 0.00, 1.20, fx_vclight , light.8 = 4, -21.00, 0.00, 2.10, fx_vclighth , light.9 = 4, -27.00, 0.00, 2.10, fx_vclighth , light.10 = 4, -33.00, 0.00, 2.10, fx_vclighh , [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 15 // 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 system_type = 1 [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_s, 1 [fuel] Center1 = -41.4, 0.0, -1.5, 400.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -36.3, -8.0, -1.8, 300.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -36.3, 8.0, -1.8, 300.0, 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 [airplane_geometry] wing_area = 350.0 //Square feet wing_span = 45.8 //Feet wing_root_chord = 9.9 //Feet wing_dihedral = 3.0 //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 = 13.5 //Degrees, wing leading edge wing_pos_apex_lon = -31.5 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = -2.0 //Feet, vertical distance from reference point, positive going up htail_area = 54.0 //Square feet htail_span = 17.2 //Feet htail_pos_lon = -59.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 8.5 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.0 //Degrees htail_sweep = 25.0 //Degrees, horizontal tail leading edge vtail_area = 52.0 //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 = 3.1 //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 auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 118.0 //Knots True (KTAS) full_flaps_stall_speed = 106.0 //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= 1500.0 autothrottle_available= 1 autothrottle_arming_required= 1 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 //use_no_default_bank=1 //use_no_default_pitch=1 [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 [pitot_static] pitot_heat=1 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [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 [GPWS] max_warning_height = 1000 sink_rate_fpm = -1500 excessive_sink_rate_fpm = -2000 climbout_sink_rate_fpm = -100 flap_and_gear_sink_rate_fpm= -100 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000