[fltsim.0] title=Learjet 45 American Edition sim=Lear45 model= panel= sound= texture= kb_checklists=Lear45_check kb_reference=Lear45_ref atc_type=Learjet atc_id_enable=1 atc_id=HB-NEH editable=0 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. [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 [WEIGHT_AND_BALANCE] 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 //Pssngr 1 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 170, -22.5, 1.2, 0.0 //Pssngr 2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 170, -26.7, -1.2, 0.0 //Pssngr 3 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 170, -26.7, 1.2, 0.0 //Pssngr 4 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 170, -30.9, -1.2, 0.0 //Pssngr 5 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = 170, -30.9, 1.2, 0.0 //Pssngr 6 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8 = 170, -35.1, -1.2, 0.0 //Pssngr 7 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9 = 170, -35.1, 1.2, 0.0 //Pssngr 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) empty_weight_roll_MOI=45000.000000 empty_weight_pitch_MOI=50000.000000 empty_weight_yaw_MOI=70000.000000 empty_weight_coupled_MOI=3300.000000 [jet_engine] thrust_scalar = 1.0 [General] performance=Vitesse de croisière Mach 0,81\nAutonomie maximale 2 200 mn.\nPlafond \nopérationnel 51 000 pieds\nPoids brut \nmaximum\t 9 264 livres\nCapacité\t jusqu'à 9 \n\t passagers\nCharge utile 1 200 kg\n [fuel] Center1=-41.360000,0.000000,-1.500000,359.000000,0.000000 LeftMain=-36.300000,-10.000000,-1.500000,268.500000,0.000000 RightMain=-36.300000,10.000000,-1.500000,268.500000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=312.000000 wing_span=45.833333 wing_root_chord=7.250000 wing_dihedral=2.499390 wing_incidence=0.000000 wing_twist=-1.499634 oswald_efficiency_factor=0.847453 wing_winglets_flag=1 wing_sweep=0.000000 wing_pos_apex_lon=-34.480830 wing_pos_apex_vert=0.000000 htail_area=67.000000 htail_span=17.166667 htail_pos_lon=-59.083333 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=42.000000 vtail_span=7.389181 vtail_sweep=0.000000 vtail_pos_lon=-55.000000 vtail_pos_vert=4.083333 elevator_area=16.985000 aileron_area=13.477000 rudder_area=7.275000 elevator_up_limit=16.999658 elevator_down_limit=15.498508 aileron_up_limit=18.002334 aileron_down_limit=18.002334 rudder_limit=30.000070 elevator_trim_limit=15.000035 spoiler_limit=59.988681 spoilerons_available=1 aileron_to_spoileron_gain=4.600000 min_ailerons_for_spoilerons=4.984733 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,-11.166667,0.000000,-4.416667,1181.102362,0.000000,0.635551,46.800000,0.241091,2.500000,0.775623,10.000000,10.000000,0.000000,0.000000,0.000000 point.1=1.000000,-37.250000,-4.750000,-4.916667,1574.803150,1.000000,0.635551,0.000000,0.504407,2.500000,0.532165,9.000000,9.000000,2.000000,0.000000,0.000000 point.2=1.000000,-37.250000,4.750000,-4.916667,1574.803150,2.000000,0.635551,0.000000,0.504407,2.500000,0.532165,9.000000,9.000000,3.000000,0.000000,0.000000 point.3=2.000000,-37.833333,-23.916667,-3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-37.833333,23.916667,-3.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-57.166667,0.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,-11.416667,0.000000,-1.500000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=-0.752563 static_cg_height=4.409246 [Flaps.0] type=1 span-outboard=0.500000 extending-time=7.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-42.833333,-4.833333,0.833333 Engine.1=-42.833333,4.833333,0.833333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002500 inlet_area=4.289500 rated_N2_rpm=29920.000000 static_thrust=3500.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=100.000000 full_flaps_stall_speed=80.000000 cruise_speed=413.519178 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=-17.108985,-1.307210,1.640420 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=3,0
