Exterior
Overall Snow White with Exxon Gray, Skyhawk Gray and Jay Gray stripes.
Interior
This well appointed interior is overall Beige / Cherry. The fireblocked passenger seats are in Willow Townsend Leather. The headliner is Raffia leather and window reveals are covered in Design Tex fabric. Sidewalls are in Paprika fabric with the carpet in Kalogridis Dark Cherry Tip Shear. The cabinetry is finished in Block Mottle Makore high gloss wood veneer with Fine Antique Gold hardware.
Cabin Configuration
Ten passenger seats are arranged in a double club configuration with dual RH Fwd side-facing seats. Work surfaces consist of four executive tables. Storage includes dual navigation chart cases, a LH Fwd refreshment center, A RH Fwd closet and an aft cabin bulkhead closet. The lavatory contains a non-belted externally serviceable toilet, a vanity cabinet and sliding divider doors. 110V outlets are located in the cabin and cockpit. Cabin electronics consist of an optional Aircell Axxess II phone system, dual DVD players, XM Radio, and Airshow 410 system with monitors located in the window reveals.
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, ADF and Mode S Enhanced Transponders.
ADDITIONAL AVIONICS:
• Dual Honeywell Primus Epic FMS
• Honeywell KHF -1050 (single with provisions for second)
• L3 FA-2100 Flight Data Recorder
• Aircell Axxess II Satellite Telephone
• Airshow 410
• Honeywell Data Management Unit
• Coltech CSD-714 SELCAL
• L3 FA-2100 CVR
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, Extended Range Oxygen System, EROS Crew Oxygen Masks, Dual DVD Player, XM Radio, XM Weather, Epic Phase 4 Chart Installation.