FS2002//Falcon 50 CAEA config file: Copyright Y Lavigne - F Banting - R Young
//IMPORTANT!!!!!! This file is ESSENTIAL to run the Falcon 50 accurately - please do NOT change parameters within

[fltsim.0]
title=Falcon50full
sim=Fal50caea2
model=
panel=
sound=
texture=
kb_checklists=Fal50caea2_CHECK
kb_reference=Fal50caea2_REF
atc_id=F-CAEA
ui_manufacturer=Dassault
ui_type=Falcon 50
ui_variation=full
visual_damage=1
description=Dassault-Aviation/Falcon 50/1976/ full model including virtual interior


[fltsim.1]
title=Falcon50light
sim=Fal50caea2
model=light
panel=light
sound=
texture=
kb_checklists=Fal50caea2_CHECK
kb_reference=Fal50caea2_REF
atc_id=F-CAEA
ui_manufacturer=Dassault
ui_type=Falcon 50
ui_variation=Light
visual_damage=1
description=Dassault-Aviation/Falcon 50/1976/ light model without virtual interior



[General]
atc_type=Dassault
atc_model=Falcon 50
editable=0
performance=Falcon 50 Corporate Jet\nDesigned by Yannick Lavigne \nGauges by Fred Banting\nAerodynamics by Rob Young \nCopyright 2001 Y. Lavigne R.Young F. Banting\nCommercial use of data and or likeness of airfile\nand aircraft strictly prohibited.\n\nPlease see documentation for performance specifications

[pitot_static]
vertical_speed_time_constant = 1.43


[WEIGHT_AND_BALANCE]

max_number_of_stations=14

station_load.0=150, 12, -1.2, 0.0         //Pilot    Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=150, 12,  1.2, 0.0         //Co-Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=160, 6.0, -1.2, 0.0         //Pssngr 1 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=160, 6.0,  1.2, 0.0         //Pssngr 2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=120, 0.0,  -1.2, 0.0         //Pssngr 3 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=120, 0.0,  1.2, 0.0         //Pssngr 4 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=160, -6.0, -1.2, 0.0         //Pssngr 5 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7=160, -6.0, 1.2, 0.0         //Pssngr 6 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=140, -10.0, -1.2, 0.0         //Pssngr 7 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9=140, -10.0, 1.2, 0.0         //Pssngr 8 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10=90, 6.0,  -1.2, 0.0       //Pssngr 9 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11=90, 6.0, 1.2, 0.0         /Pssngr 10 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.12=60, -8.0, 2.0, 0.0         //Baggage2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.13=60, -8.0, 2.0, 0.0         //Baggage2 Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=1.000000,0.000000,0.000000
empty_weight=21870.000000
empty_weight_roll_MOI=800000.000000
empty_weight_pitch_MOI=220000.000000
empty_weight_yaw_MOI=100000.000000
empty_weight_coupled_MOI=1000.000000
max_gross_weight=38800.00

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0


[forcefeedback]
stick_shaker_magnitude=2000		; 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

[fuel]
Center1=1.300000,0.000000,0.000000,765.000000,0.000000
LeftMain=1.000000,-6.000000,0.000000,765.000000,0.000000
RightMain=1.000000,6.000000,0.000000,765.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=720.000000
wing_span=58.333333
wing_root_chord=13.333333
wing_dihedral=2.999268
wing_incidence=1.8
wing_twist=0.0
oswald_efficiency_factor=0.74 
wing_winglets_flag=0
wing_sweep=20.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=40.000000
htail_span=10.833333
htail_pos_lon=-33.333333
htail_pos_vert=0.000000
htail_incidence=-0.763550     // -0.763550
htail_sweep=0.000000
vtail_area=46.000000
vtail_span=7.733046
vtail_sweep=0.000000
vtail_pos_lon=-33.333333
vtail_pos_vert=5.833333
elevator_area=50.000000
aileron_area=11.000000
rudder_area=25.000000
elevator_up_limit=35.0
elevator_down_limit=30.0
aileron_up_limit=23.491270
aileron_down_limit=23.491270
rudder_limit=21.772396
elevator_trim_limit=24.0
spoiler_limit=57.295780
spoilerons_available=0
aileron_to_spoileron_gain=4.600000
min_ailerons_for_spoilerons=49.847328
min_flaps_for_spoilerons=0.000000


//0  Class
//1  Longitudinal Position    (feet)
//2  Lateral Position             (feet)
//3  Vertical Position            (feet)
//4  Impact Dmge Thresh     (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 Comp Ratio
//10 Damping Ratio               (0=Undamped, 1=Critically Damped)
//11 Extension Time              (seconds)
//12 Retraction Time             (seconds)
//13 Sound Type
[contact_points]
point.0=1.0,   28.3,  0.0,   -7.00,    1181,   0.0,  0.76, 47.0,  0.26,   1.2,   0.5,  10, 10,  0,
point.1=1.0,  -1.0,  -19.16, -6.85,  1574,   1.0,  0.76,  0.0,  0.25,    2.50,  0.38,  11, 11,  2, 
point.2=1.0,  -1.0,   19.16, -6.95,  1574,   2.0,  0.76,  0.0,  0.25,    2.50,  0.38,  11, 11,  3,
point.3=2.0,  -3.33, -23.9,  -3.0,     787,    0.0,  0.0,    0.0,    0.0,    0.0,    0.0,    0,  0,   5,
point.4=2.0,  -3.33,  23.9,  -3.0,     787,    0.0,  0.0,    0.0,    0.0,    0.0,    0.0,    0,  0,   6,  
point.5=2.0, -22.66,  0.0,    0.0,     787,    0.0,  0.0,    0.0,    0.0,    0.0,    0.0,    0,  0,   9, 
point.6=2.0,  23.08,  0.0,  -1.50,    787,    0.0,  0.0,    0.0,    0.0,    0.0,    0.0,    0,  0,   4, 
static_pitch=0.1
static_cg_height=6.908113

[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=20.0,0.000000
flaps-position.2=47.0,0.000000
flaps-position.3=88.0,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-5.000000,0.000000,3.333333
Engine.1=-5.000000,-3.000000,0.833333
Engine.2=-5.000000,3.000000,0.833333
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002500 //0.002500
inlet_area=1.40000
rated_N2_rpm=29920.000000
static_thrust=3300.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=112.000000
full_flaps_stall_speed=89.600000
cruise_speed=307.391124

[keyboard_response]
elevator=100.000000,180.000000
aileron=100.000000,180.000000
rudder=100.000000,200.000000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[Views]
eyepoint=15.70,-1.45,2.4

[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=98.5
pitch_takeoff_ga=9.000000
use_no_default_pitch=1

[direction_indicators]
direction_indicator.0=3,0

[Radios]
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

[LIGHTS]
light.0=3,   -7.7, -31.2,  -2.1, fx_navred ,
light.1=3,   -7.7,  31.2,  -2.1, fx_navgre ,
light.2=2,   -8,  31.4,  -2.1, fx_strobe ,
light.3=2,   -8, -31.4,  -2.1, fx_strobe ,
light.4=1,  -25.2,   0.00,  17.7, fx_beaconh ,
light.5=3, -24.2,   0.00,  8.37, fx_navwhih ,
light.6=2,  4.61,   0.00, -3.62, fx_beaconb ,
light.7=5,  11.45, -2.10, -2.50, fx_landing.fx ,
light.8=5,  11.45, 2.10, -2.50, fx_landing.fx ,