Exterior

Interior

An overall gray interior. The fireblocked seats are Asphalt Townsend leather. The headliner and window reveals are covered in gray fabric. The lower sidewalls are Wavy Diamond Townsend leather. The carpet is Glacier Kalogridis cut pile. Cabinetry throughout is finished in Bird’s Eye Maple with Smoked Satin Nickel plating.  

Cabin Configuration

Seating for nine passengers consisting of a center club configuration, a RH FWD two-place side-facing couch, and a removable LH side-facing seat in the aft cabin. Internal storage provided by dual navigation chart cases, a LH FWD refreshment center, a RH FWD closet, and an aft bulkhead closet. An Aircell AxxessII phone system with wireless high-speed internet allows for communications. Electricity provided by 110 VAC outlets located in the cockpit and in the cabin. A RosenView moving map display is flush-mounted on the RH FWD cabinet.

Avionics

PRIMARY AVIONICS:
• Collins ProLine 21 Integrated Flight Director / Autopilot and EFIS with 4 8x10 AMLCDs
• Collins ProLine 21 CNS Radios with dual COMM (8.33kHz), dual NAV, single DME, single ADF, dual Radio Tuning Units (RTUs), and dual TDR-94D Mode S Diversity Transponders with Enhanced Surveillance.
 

ADDITIONAL AVIONICS:
• Dual Collins FMS-3000
• Collins HF-9031A w/SELCAL
• Honeywell Mark V EGPWS
• L-3 Communications FA2100 CVR
• Performance Database
• Artex C406-N ELT (Three Frequency)
• XM WX
• Collins TWR-850 Turbulence Weather Radar
• Jeppesen Electronic Charts
• Collins TCAS-4000 (TCAS II Change 7)
 

Powerplant

Two Pratt & Whitney Canada PW545C turbofan engines are installed on the Citation XLS+, one on each side of the rear fuselage in easily accessible nacelles. The PW545C produces a static takeoff thrust of 4,119 pounds (18.32kN) at sea level, up to 77°F (25°C) and has a bypass ratio of 3.8 to 1. Major maintenance intervals are 2,500 hours for hot section inspection and 5,000 hours for overhaul.

Dual channel Full Authority Digital Electronic Controls (FADECs) provide automation and efficiency in engine management. Detents in the throttle quadrant (takeoff, climb, cruise) permit optimal power settings based on ambient conditions for each phase of flight. The system also provides time-limited dispatch (TLD), engine protection, synchronization, and diagnostic capability.

Hydraulically actuated, target-type thrust reversers are attached to each engine. The effect of the thrust reversers on runway performance is accounted for under some conditions.

A continuous loop fire detection system monitors the nacelle area to detect and warn if a fire occurs. A two-shot fire extinguishing system is supplied.
 

The Honeywell RE100(XL) APU is installed in the tail-cone equipment bay. The APU supplies bleed air for pressurization and air conditioning, electrical power for engine assisted air starts, and other benefits. It is certified for use in flight up to 30,000 feet.
 

Installed Equipment

RVSM Capable, APU, Thrust Reversers, Cockpit Speaker Mute Switch, Tail Flood Lights, Pulse Lights, 77.1 Cubic Foot Oxygen System.