[fltsim.0] title=BD100Challenger sim=FSDS object model= panel= sound= texture= kb_checklists= atc_id=N456LJ ui_manufacturer=Bombardier ui_type=BD100 ui_variation=Challenger300 description=The first all-new Learjet since Bill Lear rolled the model 23 off the line in the 1960s, this computer-designed airplane is a fast, high altitude flyer. Certified up to 51,000 ft (15,545 m), the Learjet 45 often cruises above standard airliner altitudes. After transitioning in Flight Simulator from the complex single-engine airplanes to the King Air, move into piloting jets with the Lear. See the Aircraft Information section of Help for tips on flying this aircraft. [General] atc_type=Learjet atc_model= 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" [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 = .5 parasite_drag_scalar = .5 induced_drag_scalar = .5 elevator_effectiveness = .5 aileron_effectiveness = .5 rudder_effectiveness = .5 pitch_stability = .5 roll_stability = .5 yaw_stability = .5 elevator_trim_effectiveness = .5 aileron_trim_effectiveness = .5 rudder_trim_effectiveness = .5 [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 = .6 //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 = 400 //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=28.0 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