[fltsim.0] title=Dassault Falcon 100 sim=Dassault Falcon 100 model= panel= sound= texture= checklists= atc_id=N561F ui_manufacturer=Dassault ui_type=Falcon 100 ui_variation=White with Red description=First flown in 1970 as the Falcon 10, the 100 has a higher take-off weight and a fourth cabin window on the starboard side. This one was made with FSDS by ABACUS. [General] atc_type=Falcon atc_model=100 editable=1 performance=Length: 48.1 ft\nHeight: 15.2 ft\nWingspan: 46.2 ft\nPassengers: 8\nCargo: 1305 kg\nRange: 2900 km\nDesigner: Chuck Dome\nDate: March, 2002 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=9000.000000 empty_weight_roll_MOI=45000.000000 empty_weight_pitch_MOI=100000.000000 empty_weight_yaw_MOI=70000.000000 empty_weight_coupled_MOI=3300.000000 [fuel] Center1=0.000000,0.000000,0.000000,100.000000,0.000000 LeftMain=-1.666667,-10.416667,-1.500000,275.000000,0.000000 LeftAux=5.250000,0.000000,0.000000,175.000000,0.000000 RightMain=-1.666667,10.416667,-1.500000,275.000000,0.000000 RightAux=5.250000,0.000000,0.000000,175.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=365.000000 wing_span=39.583333 wing_root_chord=9.166667 wing_dihedral=2.499390 wing_incidence=0.000000 wing_twist=-1.499634 oswald_efficiency_factor=1.329205 wing_winglets_flag=1 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=67.000000 htail_span=17.166667 htail_pos_lon=-24.583333 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=-20.500000 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=1.000000,25.000000,0.000000,-4.6,1181.102362,0.000000,0.608839,48.000000,0.100000,2.500000,0.938457,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-1.250000,-4.750000,-5.1,1574.803150,1.000000,0.608839,0.000000,0.408592,2.500000,0.591278,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-1.250000,4.750000,-5.1,1574.803150,2.000000,0.608839,0.000000,0.408592,2.500000,0.591278,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-3.333333,-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,-3.333333,23.916667,-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,-22.666667,0.000000,0.000000,787.401575,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,23.083333,0.000000,-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=5.000000 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=-8.333333,-4.833333,0.833333 Engine.1=-8.333333,4.833333,0.833333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=4.932000 rated_N2_rpm=29920.000000 static_thrust=2994.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=100.000000 full_flaps_stall_speed=80.000000 cruise_speed=560.962883 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=13.0,-1.26,2.4 [autopilot] autopilot_available=1 flight_director_available=0 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 use_no_default_bank=1 [direction_indicators] direction_indicator.0=3,0 [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 [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