Exterior
Overall snow white with fawn, platinum and chestnut brown stripes.
Interior
Overall elegant beige scheme. The fireblocked passenger seats are in Taupe colored leather. The window reveals are a light beige-colored vinyl material and the lower sidewalls are textured beige fabric. The carpet is beige colored cut pile. The cabinetry is East Indian Laurel wood veneer and the plating is Antique Bronze.
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 forward left-hand refreshment center, right-hand closet, executive & slimline tables, seat back pockets on all seats except the entrance, and storage drawers under four seats. The lavatory includes a left hand belted, flushing toilet with a carry-out tank, along with an aft centerline closet.
Avionics
PRIMARY AVIONICS:
- Honeywell P-1000 Integrated Flight Director & Autopilot System, 3-tube 8x7” EFIS.
- Honeywell Primus II Radios with Dual Comm, Dual Nav with 8.33 spacing, ADF, Dual DME, Dual RMI & Dual Mode S Enhanced Transponders.
ADDITIONAL AVIONICS:
- Dual Universal UNS-1CSP FMS with permanent DTU
- Honeywell Primus 880 Stabilized Color Radar
- Collins ALT-55 Radio Altimeter
- Honeywell TCAS II
- Honeywell Mark V EGPWS
- Artex e frequency ELT with Nav. Interface
- Universal UL-701 Unilink
- TT-3000 Aero-M SATCOM
- Dual DVD Player
Powerplant
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, APU, Thrust Reversers, 76 cu. Ft. Oxygen, Right Hand Landing Gear Control, Monorail Sunvisor, Nickel Cadmium Battery, Airshow 400.
