[fltsim.0] title=Cessna Citation Excel - Citation Shares (N556CS) sim=XLS model= panel=FP sound= texture=FIV_N556CS kb_checklists= atc_id=N556CS atc_airline=Five Star atc_flight_number=231 atc_parking_types=RAMP,GATE atc_parking_codes=FIV ui_manufacturer=Cessna ui_type=Citation XLS+ ui_variation=Citation Shares - N556CS description=Aryus Works. It's the newest chapter in one of business aviation's most phenomenal success stories. And it's absolutely magnificent. With the incomparable Citation XLS+, we've taken the world's best-selling business jet and made it even better. Among the enhancements are some of the industry's most desired avionics, full-authority digital engine controls (FADEC), an upgraded cockpit, wider passenger seats and a more streamlined profile. The XLS+ is your opportunity to do for your business what we did with the aircraft itself - take it swiftly and surely to the next level and beyond. \n Model and textures by Alex Guedes (Aryus Works)\n Citation Shares (N556CS) repaint \n by Jeffrey S. Bryner [General] atc_type=Cessna atc_model=C560 editable=1 performance=Cruise Speed\t.76 Mach\nMaximum Range\t1,858 nm\nService Ceiling\t45,000 ft\nMax Takeoff Weight\t20,400 lb\nSeating\t\t6 to 8\ Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=20400.0 // (pounds) empty_weight=11910.0 // (pounds) reference_datum_position=0.00, 0.00, 0.00 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position=-1.0, 0.00, 0.0 // -3.9 (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="170, 19.0, 0, 0.0, Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.1="170, 19.0, 0, 0.0, Co-Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.2="340, 11.5, 0, 0.0, Passenger 1 & 2" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.3="170, -10.5,0, 0.0, Passenger 3 & 4" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.4="0, -20.7,0, 0.0, Passenger 5 & 6" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.5="0, -30.7,0, 0.0, Passenger 7 & 8" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) station_load.6="11, -40.9,0, 0.0, Cargo" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet) ;Moments of Inertia empty_weight_pitch_MOI=49967 empty_weight_roll_MOI=71681 empty_weight_yaw_MOI=128000 empty_weight_coupled_MOI=0 [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 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.39, -5.5, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-8.39, 5.5, 3.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.2 //Scalar for fuel flow efficiency min_throttle_limit=-0.18 //Minimum percent throttle. Generally negative for turbine reverser [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=2.9 //Square Feet, engine nacelle inlet area rated_N2_rpm=32740 //RPM, second stage compressor rated value static_thrust=4220 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [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, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 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 //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) [contact_points] point.0=1, 21.8, 0.00, -4.23, 1181.1, 0, 0.9349, 62.600, 0.200, 2.5, 0.600, 7.0, 7.0, 0.000, 0.000, 0.000 point.1=1, -2.4, -6.95, -5.11, 1574.8, 1, 1.6349, 0.0, 1.090, 1.3, 1.446, 9.0, 9.0, 2, 260.0, 260.0 point.2=1, -2.4, 6.95, -5.11, 1574.8, 2, 1.6349, 0.0, 1.090, 1.3, 1.446, 9.0, 9.0, 2, 260.0, 260.0 point.3=2, -0.8, -28.4, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -0.8, 28.4, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -24.6, 0.00, 3.20, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 29.0, 0.00, -1.08, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 max_number_of_points=21 static_pitch=-1.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=5.16 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [ground_reaction] main_gear_static_compression=1.00 center_gear_static_compression=0.5 main_gear_damping_ratio=0.55 center_gear_damping_ratio=0.7 [gear_warning_system] gear_warning_available=1 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=5.0 //Flap angle that activates warning at idle flap_limit_power=25.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.75 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=16.7, -0.98, 2.9 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps] type=1 // 1 - tail, 2 - lead span-outboard=0.7 // 0.0 .. 1.0 extending-time=10 // seconds flaps-position.0=0 // degrees flaps-position.1=7 // degrees flaps-position.2=15 // degrees // KIAS flaps-position.3=35 // degrees blowout-speed=300 // KIAS lift_scalar=0.51 drag_scalar=0.91 pitch_scalar=0.51 system_type=1 //Hydraulic [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cockpit light.0=3, -0.43, -28.4, -0.0, fx_navredh , light.1=3, -0.43, 28.4, -0.0, fx_navgreh , light.2=3, -25.371428, 0.00, 2.10, fx_strobe , light.3=2, -0.65, -28.380158, -0.0, fx_strobeh , //Leftwing strobe light.4=2, -0.65, 28.380158, -0.0, fx_strobeh , //Rightwing strobe light.5=4, 15.5, 0.0, 3.9 , fx_vclighth, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [airplane_geometry] wing_area=369.7 //Square feet wing_span=55.8 //Feet wing_root_chord=10.7 //Feet wing_dihedral=6.7 //Degrees wing_incidence=1.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.6 //Measure of lift effeciency of wing 0.816 wing_winglets_flag=0 //Are winglets available? wing_sweep=6.0 //Degrees, wing leading edge wing_pos_apex_lon=2.7 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=67.0 //Square feet htail_span=10.85 //Feet htail_pos_lon=-24.82 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=5.084 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=10.0 //Degrees, horizontal tail leading edge vtail_area=42.0 //Square feet vtail_span=9.0 //Feet, tip to body vtail_sweep=37.0 //Degrees, vertical tail leading edge vtail_pos_lon=-18.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up elevator_area=17.0 //Square feet aileron_area=13.5 //Square feet rudder_area=18.3 //Square feet elevator_up_limit=19.0 //Degrees elevator_down_limit=15.5 //Degrees aileron_up_limit=19.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=22.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=65.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=3.0 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=102.0 //Knots True (KTAS) full_flaps_stall_speed=82.6 //Knots True (KTAS) cruise_speed=440.7 //Knots True (KTAS) max_mach=0.85 max_indicated_speed=295 //Red line (KIAS) [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150.0, 250.0 aileron=150.0, 250.0 rudder=150.0, 250.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.0 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 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=9.00 nav_integrator_control=0.25 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] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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=2 stick_shaker=1 [direction_indicators] direction_indicator.0=3,0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 //+++++++++++++++++++++++++++++++++++++++++++++++++ //+++ Those following elements where modified //+++ in aim to let the gauges working //+++++++++++++++++++++++++++++++++++++++++++++++++ [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 attitude_indicator.1=2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 turn_indicator.1=1,0 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [altimeters] altimeter.0=1 altimeter.1=1 [fuel] LeftMain= 0.0,-7.5, -0.0, 503.00, 0.0 RightMain=0.0, 7.5, -0.0, 503.00, 0.0 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 electric_pump=1 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [Radios] ;/ Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1
