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=0
description=Dassault-Aviation\/Falcon 50\/1976\/ full model including virtual interior
atc_heavy=0
atc_airline=
atc_flight_number=


[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=0
description=Dassault-Aviation/Falcon 50/1976/ light model without virtual interior


[General]
atc_type=DASSAULT
atc_model=Falcon 50
editable=1
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=0.4


[WEIGHT_AND_BALANCE]

max_number_of_stations=14

station_load.0= 150.000, 12.000, -1.200, 0.000
station_load.1= 150.000, 12.000, 1.200, 0.000
station_load.2= 160.000, 6.000, -1.200, 0.000
station_load.3= 160.000, 6.000, 1.200, 0.000
station_load.4= 120.000, 0.000, -1.200, 0.000
station_load.5= 120.000, 0.000, 1.200, 0.000
station_load.6= 160.000, -6.000, -1.200, 0.000
station_load.7= 160.000, -6.000, 1.200, 0.000
station_load.8= 140.000, -10.000, -1.200, 0.000
station_load.9= 140.000, -10.000, 1.200, 0.000
station_load.10= 90.000, 6.000, -1.200, 0.000
station_load.11= 90.000, 6.000, 1.200, 0.000
station_load.12= 60.000, -8.000, 2.000, 0.000
station_load.13= 60.000, -8.000, 2.000, 0.000
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 1.000, 0.000, -2.000
empty_weight= 22500.000
empty_weight_roll_MOI= 800000.000
empty_weight_pitch_MOI= 700000.000
empty_weight_yaw_MOI= 200000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 38800.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
cruise_lift_scalar=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=9.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.7
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=9.000


[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=05900		; 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

//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
//14 Airspeed limit for retraction     (KIAS)
//15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0= 1.000, 25.300, 0.000, -7.300, 1874.000, 0.000, 2.500, 31.000, 0.500, 2.500, 0.700, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1.000, -2.000, -7.000, -7.450, 1874.000, 1.000, 3.260, 0.000, 0.840, 2.500, 0.700, 11.000, 11.000, 2.000, 180.000, 740.877
point.2= 1.000, -2.000, 7.000, -7.490, 1874.000, 2.000, 3.260, 0.000, 0.840, 2.500, 0.700, 11.000, 11.000, 3.000, 180.000, 740.877
point.3= 2.000, -3.330, -23.900, -3.000, 1787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.330, 23.900, -3.000, 1787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

point.5= 2.000, -22.660, 0.000, -3.400, 1787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

point.6= 2.000, 23.080, 0.000, -3.500, 1787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch= 0.000
static_cg_height= 7.130

[Reference Speeds]
flaps_up_stall_speed= 112.000
full_flaps_stall_speed= 89.600
cruise_speed= 307.391

[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=7.83,-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 ,

[fuel]
Center1= 1.300, 0.000, 0.000, 765.000, 0.000
LeftMain= 1.000, -6.000, 0.000, 765.000, 0.000
RightMain= 1.000, 6.000, 0.000, 765.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 719.000
wing_span= 58.333
wing_root_chord= 7.250
wing_dihedral= 2.499
wing_incidence= 0.100
wing_twist= 0.000
oswald_efficiency_factor= 0.883
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.019
wing_pos_apex_vert= 0.000
htail_area= 80.000
htail_span= 10.833
htail_pos_lon= -33.333
htail_pos_vert= 0.000
htail_incidence= 1.500
htail_sweep= 0.000
vtail_area= 46.000
vtail_span= 7.733
vtail_sweep= 0.000
vtail_pos_lon= -33.333
vtail_pos_vert= 5.833
elevator_area= 16.985
aileron_area= 13.477
rudder_area= 7.275
elevator_up_limit= 17.000
elevator_down_limit= 15.499
aileron_up_limit= 18.002
aileron_down_limit= 18.002
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 4.600
min_ailerons_for_spoilerons= 4.985
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 1
Engine.0= -5.000, 0.000, 3.333
Engine.1= -5.000, -3.000, 0.833
Engine.2= -5.000, 3.000, 0.833
fuel_flow_scalar= 1.000

[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 1.400
rated_N2_rpm= 29920.000
static_thrust= 3300.000
afterburner_available= 0
reverser_available= 1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.331, 0.000
flaps-position.2= 34.662, 0.000
flaps-position.3= 65.992, 0.000

[jet_engine]
thrust_scalar=1.000