// PREMIER AIRCRAFT DESIGN
// DASSAULT FALCON 7X for FS2004
// JP BRISARD
// FD adjusted DC & BM March 30 2009
// Copyright 2009
[fltsim.0]
title=Falcon7X_fix10
sim=Falcon7x
model=
panel=falc79
sound=falc
texture=cs-tly
kb_checklists=falcon7X_check
kb_reference=falcon7X_ref
atc_id=CS-TLY
atc_airline=
atc_flight_number=
atc_heavy=1
ui_manufacturer=Dassault
ui_type=Falcon 7X
ui_variation=CS-TLY
visual_damage=0
description=Falcon\nLong Range Business Travel aircraft
[General]
performance=Power: 3 Pratt&Whitney PW4462 Turbofans @ 62,000lbs Thrust ea\nCruise Speed\tMach .81\nMaximum Range\t5,700 nm\nService Ceiling\t50,000 ft\nMax Takeoff Weight\t63,600 lb
atc_type=Dassault
atc_model=Falcon
[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]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=2, -20.619, -40.737, -0.193, fx_strobeh ,
light.1=2, -20.619, 40.737, -0.193, fx_strobeh ,
light.2=1, -18.470, 0.00, 10.132, fx_padbeaconh ,
light.3=1, 2.150, 0.00, -4.7, fx_padbeaconh ,
light.4=4, 25.80, -1.00, 2.36, fx_vclightwhite ,
light.5=4, 25.80, 1.00, 2.36, fx_vclightwhite ,
light.6=4, 22.27, 0.00, 2.36, fx_vclighth ,
light.7=4, 11.54, 0.00, 2.5, fx_vclighth ,
light.8=4, 5.54, 0.00, 2.5, fx_vclighth ,
light.9=4, -2.2, 0.00, 2.5, fx_vclighth ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=9000
autothrottle_takeoff_ga=1
pitch_takeoff_ga=10
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[airplane_geometry]
wing_area=865.000
wing_span=87.000
wing_root_chord=11.000
wing_dihedral=2.000
wing_incidence=2.500
wing_twist=-1.000
oswald_efficiency_factor=1.000
wing_winglets_flag=1
wing_sweep=35.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=231.000
htail_span=27.000
htail_pos_lon=-49.000
htail_pos_vert=0.000
htail_incidence= -3.000
htail_sweep=20.000
vtail_area=102.000
vtail_span=11.600
vtail_sweep=0.000
vtail_pos_lon=-48.000
vtail_pos_vert=6.000
elevator_area=57.500
aileron_area=25.000
rudder_area=32.300
elevator_up_limit=28.000
elevator_down_limit=20.000
aileron_up_limit=20.000
aileron_down_limit=15.000
rudder_limit=24.000
elevator_trim_limit=20.000
spoiler_limit=60.000
spoilerons_available=1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=10.000
min_flaps_for_spoilerons=0.000
[pitot_static]
vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI
[flight_tuning]
cruise_lift_scalar=1.150
parasite_drag_scalar=0.900
induced_drag_scalar=0.850
pitch_stability=3.500
roll_stability=2.000
yaw_stability=1.500
elevator_effectiveness= 1.30
aileron_effectiveness= 1.00
rudder_effectiveness= 1.00
elevator_trim_effectiveness=1.00
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
//[Moments of Inertia]
//empty_weight_pitch_MOI = 60000
//empty_weight_roll_MOI = 55000
//empty_weight_yaw_MOI = 80000
//empty_weight_coupled_MOI = 0.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 12 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.5
drag_scalar = 1.5
pitch_scalar= 2.0
[flaps.1] //Inboard Leading Edge Flaps
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.5
drag_scalar = 2.00
pitch_scalar= 1.00
[flaps.2] //Outboard Leading Edge Slat
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 4 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 0.5 //
flaps-position.4 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.5
drag_scalar = 2.00
pitch_scalar= 1.00
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
[SMOKESYSTEM]
smoke.0=-28.750, 0.000, 10.00, fx_turbo_exhaust.fx
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (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 Compression 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)
point.0=1.000, 25.333, 0.000, -6.447, 1574.803, 0.000, 0.882,55.440, 0.274, 2.500, 0.678, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -10.000, -7.083, -6.460, 1574.803, 1.000, 0.882, 0.000, 0.274, 2.500, 0.678, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -10.000, 7.083, -6.460, 1574.803, 2.000, 0.882, 0.000, 0.274, 2.500, 0.678, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -12.333,-35.333, 2.167, 1574.803, 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, -12.333, 35.333, 2.167, 1574.803, 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, -38.333, 0.000, -1.083, 1574.803, 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, 35.333, 0.000, -1.083, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7=5.000, -30.900, 0.000, -7.300, 1600, 0.000, 0.000, 50.000, 0.000, 0.000, 1.000, 1.100, 1.500,0.000, 0.000, 0.000
static_pitch=0.000
static_cg_height=5.875
rudder_trim_effectiveness=1.000
gear_system_type=0
[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0 = 170.0, 25.00, -1.5, 0.0, Pilot //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170.0, 25.00, 1.5, 0.0, Co-Pilot //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 1020.0, 10.00, 0.0, 0.0, Passengers //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 340.0, -3.50, 0.0, 0.0, Passengers //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 80.0, -27.50, 0.0, 0.0, Aft Baggage //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight=35000.000
max_gross_weight=63600.000
CG_forward_limit=0.000
CG_aft_limit=1.000
//Moment of inertia
empty_weight_roll_MOI=342977.000
empty_weight_pitch_MOI=476240.000
empty_weight_yaw_MOI=572100.000
empty_weight_coupled_MOI=1300.000
[fuel]
Center1= 0.000, 0.000, 0.000, 1493.000, 0.000
LeftMain= 0.000, 0.000, 0.000, 1410.000, 0.000
RightMain=0.000, 0.000, 0.000, 1410.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[GeneralEngineData]
engine_type=1
Engine.0= -22.917, -10.083, 0.00,
Engine.1= -22.917, 10.083, 0.00
Engine.2= -28.750, 0.000, 0.00
fuel_flow_scalar=1.000
min_throttle_limit=-0.1000
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=7.217
rated_N2_rpm=29920.000
static_thrust=6500.000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.150
[Reference Speeds]
flaps_up_stall_speed=130.000
full_flaps_stall_speed=94.000
cruise_speed=380.000
max_indicated_speed=330.000
max_mach=0.880
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=25.00,-1.5,3.00
[exits]
number_of_exits=2
exit_rate.0=0.4 ;Percent per second
exit_rate.1=0.4
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.000
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=0.000000
flap_limit_idle=0.000000
[hydraulic_system]
normal_pressure=3000.000
engine_map=1,1,1,0
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0