Exterior
Overall snow white with antique silver, black and charcoal gray stripes.
Interior
This well appointed interior is overall beige. The fireblocked passenger seats are in crème Townsend traditional leather. The window reveals are covered in beige Design Tex fabric with the sidewalls in rosemary cloth. Carpeting is foilage Kalogridis cut pile. The cabinetry is finished in figured cherry wood veneer with satin champagne gold hardware.
Cabin Configuration
Eight passenger seats are arranged in a double club configuration. Cabin furnishings include a LH closet with CD changer, a RH extended refreshment center and four executive tables. The lavatory contains a non-belted externally serviceable toilet, a vanity cabinet and aft closet. Cabin electronics consist of an optional Aircell AST-3500 phone system, six disk CD changer and 110 volt outlets located throughout the aircraft.
Avionics
PRIMARY AVIONICS:
• Honeywell Primus Epic System with Four 8”x10” Full Color Flat Panel Displays
• Honeywell Integrated Nav and Comm System with Dual 8.33kHz VHF Comm, Nav, DME, single ADF and dual Mode S Diversity Transponders.
ADDITIONAL AVIONICS:
• Dual Honeywell Primus Epic FMS
• CAS-67 TCAS II
• Coltech CSD-714 SELCAL
• Kannad 406AF 3 Freq ELT.
• Honeywell EGPWS
• Honeywell Data Management Unit
• Aircell AST-3500 Phone System
• L3 FA-2100 CVR
• Honeywell P880 Radar
• Honeywell KHF-1050 (single with provisions for second)
Powerplant
Two Pratt & Whitney Canada, PW306C turbofan engines, rated at 5,686 lbs. static thrust each, are installed, one on each side of the rear fuselage. This engine is a 4.4 to one, high bypass ratio, twin spool design with a damage resistant wide chord fan, Behind the fan, four axial and one centrifugal compressor stages lead to a high efficiency, low emission, through-flow combustor and five turbine stages. Two stage variable inlet guide vanes and bleed-off valves are controlled by the FADEC to optimize compressor performance and engine operability. A forced exhaust mixer improves fuel burn and reduces noise. Maximum static takeoff thrust at sea level is flat rated to 5,770 pounds (25.66kN) up to 87 °F (ISA+15.5°C). Advanced alloys and cooling technologies allow for 6,000 hours between overhauls.
Engine start is accomplished electrically through a starter-generator powered by any of the following sources: the aircraft’s two batteries, the auxiliary power unit, the other running engine, or a ground power unit. Both low and high-pressure engine bleed air is extracted for anti-ice and environmental requirements. Fan air is tapped for pre-cooling of bleed air. 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 provided.
Dual channel Full Authority Digital Electronic Controls (FADECs) provide automation and efficiency in engine management. Detents in the throttle quadrant (takeoff, maximum continuous, high speed cruise) permit optimal power settings based on ambient conditions for each phase of flight. The system also provides engine protection, synchronization, and diagnostic capability.
Installed Equipment
RVSM Capable, Thrust Reversers, APU, Stereo Speaker Installation, Dropped Aisle Accent Lighting, Overhead Indirect Lighting, Precise Flight Pulse Light System, Cockpit Speaker Mute Switch, E, 76 Cubic Foot Oxygen System, EROS Crew Oxygen Masks, Six Disk CD Changer..
