[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