Exterior

Interior

The interior is an overall Beige / Brown scheme. The fireblocked passenger seats are in Champagne Townsend traditional leather. The window reveals are a Beige material with the lower sidewalls covered in light Brown patterned fabric. The carpet is Port Kalogridis Cut Pile. Cabinetry is finished in Figured Mahogany wood veneer with Rose Satin Copper plating.

Cabin Configuration

Seating for eight passengers in a center club configuration with six passenger seats and a forward side-facing two place couch. Furnishings include dual navigation chart cases, a forward LH galley, and a RH closet with B&D display. Work surfaces consist of executive & slimline tables. The lavatory contains a non-belted flushing toilet (externally serviceable), a LH entertainment cabinet with 6 disk CD player and an aft centerline closet. Additional amenities include an Aircell phone system and 110 V outlets.

Avionics

PRIMARY AVIONICS:

• Honeywell P-1000 Integrated Flight Director & Autopilot System with 3-tube 8x7” EFIS.
• Honeywell Primus II Radios with Dual Comm, Dual Nav, ADF, Dual DME, and Dual XS-852 Mode S Transponders.
 

ADDITIONAL AVIONICS:
• Universal UNS-1Csp FMS
• WX-950 Stormscope
• Honeywell KHF-950 (Provisions Only)
• Aircell ST-3100 Phone System
• Honeywell Mark V EGPWS
• B&D 2700 Cabin Display
• Honeywell P880 Color Radar
• Precise Flight Pulselight System
• Honeywell TCAS II
• Universal UL-701 Unilink
• Artex C406-2 ELT (3- Frequency)
 

Powerplant

Engines enrolled on ESP Gold Lite.

Two Pratt & Whitney Canada, PW545A turbofan engines are located, one on each side of the rear fuselage, in easily accessible nacelles.

The PW545A produces a static takeoff thrust of 3,804 pounds, sea level, up to 83 degrees Fahrenheit. Featuring a new, high efficiency exhaust nozzle, the PW545A has a bypass ration of 4.0 to 1. The PW545A uses a single channel EEC (Electronic engine control) to reduce pilot workload with a hydromechanical fuel control for redundacy. The PW545A permits a maximum engine fan speed (N1) of 100% and a maximum engine turbine speed (N2) of 101.2%.

A continuous loop fire detection system monitors the nacelle area to detect and a warn if a fire occurs. A two-shot fire extinguishing system is supplied. Target-type, hydraulically actuated thrust reversers are standard.

Installed Equipment

RVSM Capable, MSG-3 Maintenance Program, Thrust Reversers, Freon Air Conditioner, Provisions for Second FMS, 76 Cubic Foot Oxygen, Remote Cabin Temp Control, AOA Indexer, RH Landing Gear Control, Electronic Engine Chip Detector.