Exterior

Overall Matterhorn White with Cypress Blue, Platinum and Insignia Blue stripes.

Interior

The interior is an overall elegant Beige/Brown scheme. The fireblocked passenger seats are in Shadow Beige leather. The window reveals are a light Beige-colored textured fabric and the lower sidewalls are a textured Brown fabric. The carpet is Port colored cut pile. The cabinetry is Swirl Walnut wood veneer and the plating is Polished Almond Gold.

Cabin Configuration

Seating for eight passengers in a center club configuration with six passenger seats and a forward side-facing two place couch. There is a removable left-hand side-facing seat in the lavatory for a ninth passenger. The sidewall armrest at seat number 6 includes an Aircell Handset, 110vac outlet, and a fax/data outlet. There is a forward left-hand refreshment center, right-hand closet with a B&D 2700 display, executive & slimline tables, and storage drawers under four seats. The lavatory contains a non-belted flushing toilet (externally serviceable) and an aft centerline closet.

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 Mode S Transponders.

ADDITIONAL AVIONICS:
• Universal UNS-1Espw FMS
• Artex 110-4 Two Frequency ELT
• Coltech CSD-714 Selcal
• Honeywell KHF-950
• Aircell ST3100 Phone System
• Honeywell P880 Color Radar
• Precise Flight Pulselite System
• Honeywell TCAS I
• Honeywell Mark V EGPWS
• B&D2700 Cabin Information Display
 

 

Powerplant

Engines enrolled on Pratt and Whitney 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, seal level, up to 83 °F. Featuring a new, high efficiency exhaust nozzle, the PW545A has a bypass ratio 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 redundancy. 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 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, APU with Hour Meter in Cockpit, Thrust Reversers, 76 cu. Ft. Oxygen, Right Hand Landing Gear Control, Engine Chip Detector, Lead Acid Battery, Ethernet Wires between DTU and FMS, Cockpit Speaker Mute Switch.