[fltsim.0]
title=Cessna Citation Excel - Citation Shares (N556CS)
sim=XLS
model=
panel=
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\
[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
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[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
[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
[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
[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= 1
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
[direction_indicators]
direction_indicator.0=3,0
