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=falcon50 avec cockpit et cabine virtuel
sim=falcon50
model=
panel=
sound=
texture=
kb_checklists=Fal50caea2_CHECK
kb_reference=Fal50caea2_REF
atc_id=F-AQUI
ui_manufacturer=Dassault Aviation
ui_type=Falcon 50
ui_variation=Avec cockpit et cabine virtuel
visual_damage=1
description=Dassault-Aviation/Falcon 50/1976/ full model

[fltsim.1]
title=falcon50 avec cockpit virtuel
sim=falcon50
model=cv
panel=
sound=
texture=5
kb_checklists=Fal50caea2_CHECK
kb_reference=Fal50caea2_REF
atc_id=F-AQUI
ui_manufacturer=Dassault Aviation
ui_type=Falcon 50
ui_variation=Avec cockpit virtuel.
visual_damage=1
description=Dassault-Aviation/Falcon 50/1976/ 2D and 3D cockpit

[fltsim.2]
title=falcon50 avec cockpit 2D
sim=falcon50
model=2d
panel=2d
sound=
texture=
kb_checklists=Fal50caea2_CHECK
kb_reference=Fal50caea2_REF
atc_id=F-AQUI
ui_manufacturer=Dassault Aviation
ui_type=Falcon 50
ui_variation=Avec un tableau de bord 2d.
visual_damage=1
description=Dassault-Aviation/Falcon 50/1976/ 2D cockpit only


[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_gross_weight =38800
empty_weight     =21870

reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=1.000000,0.000000,0.000000

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)

;Moments of Inertia
empty_weight_roll_MOI    =80000
empty_weight_pitch_MOI   =550000
empty_weight_yaw_MOI     =120000
empty_weight_coupled_MOI =0000

[flight_tuning]
cruise_lift_scalar     =1.0
parasite_drag_scalar   =1.0
induced_drag_scalar    =1.0
elevator_effectiveness =2.0
aileron_effectiveness  =1.2
rudder_effectiveness   =1.2
pitch_stability        =1.0
roll_stability         =1.0
yaw_stability          =1.0
elevator_trim_effectiveness=0.6
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness  =1.0

[GeneralEngineData]
engine_type=1
Engine.0= -5.0,  0.0, 3.3
Engine.1= -5.0, -3.0, 0.8
Engine.2= -5.0,  3.0, 0.8
fuel_flow_scalar= 1
min_throttle_limit= -0.21

[TurbineEngineData]
fuel_flow_gain        =0.0025
inlet_area            =4.4000
rated_N2_rpm          =29920
static_thrust         =3725
//static_thrust         =4420
afterburner_available =0
reverser_available    =1

[jet_engine]
thrust_scalar = 1.0

//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]
        0       1     2       3     4    5     6     7     8     9   10   11  12  13
point.0=1.0,  24.3,   0.0, -6.70, 2481, 0.0, 0.76, 47.0, 0.20, 3.0, 0.58,  7,  7,  0,
point.1=1.0,  -1.0, -7.16, -6.80, 1874, 1.0, 0.76,  0.0, 0.20, 3.0, 0.55,  8,  8,  2, 
point.2=1.0,  -1.0,  7.16, -6.80, 1874, 2.0, 0.76,  0.0, 0.20, 3.0, 0.55,  8,  8,  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
gear_system_type=0

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.091553
flap_limit_power=80.214091
flap_limit_idle=21.772396

[brakes]
toe_brakes_scale=1.017392
parking_brake=1

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,0
normal_pressure=3000.000000

[Views]
eyepoint =22.30,-1.45,2.5 (cockpit)
eyepoint =15.70,-1.45,2.5 (cabine)

[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
light.9 = 4,  24.50,   1.80,  2.55, fx_vclight_f50
light.10= 4,  24.50,  -1.80,  2.55, fx_vclight_f50
light.11= 4,  19.00,  -0.30,  2.05, fx_vclight_f50
light.12= 4,  14.00,  -0.00,  2.05, fx_vclight_f50
light.13= 4,  10.00,  -0.00,  2.05, fx_vclight_f50
light.14= 4,   6.00,  -0.00,  2.05, fx_vclight_f50
light.15= 4,   0.80,  -0.00,  1.05, fx_vclight_f50

[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=12.0,0.000000
flaps-position.2=27,0.000000
flaps-position.3=38.0,0.000000

[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

[keyboard_response]
elevator=10.000000,10.000000
aileron=100.000000,180.000000
rudder=100.000000,200.000000

[direction_indicators]
direction_indicator.0=3,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

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

[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
electric_pump=0

[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=18.0
elevator_down_limit=18.0
aileron_up_limit=20
aileron_down_limit=20
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

[Reference Speeds]
flaps_up_stall_speed   =112.000000
full_flaps_stall_speed =89.600000
cruise_speed           =307.391124
max_indicated_speed    =369.000000
max_mach               =0.860010

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 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

[stall_warning]
type=1