// 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