Exterior
Paint touch up completed in 2009. Overall Matterhorn White with Slate Gray, Charcoal and Raspberry stripes.
Interior
Refreshed in 2009 with new window reveal material, carpet and leather work.
The interior is overall Beige / Brown. The fireblocked passenger seats are covered in Desert colored classic Townsend Leather. Window reveals are in Beige textured fabric with the lower sidewalls in Brown patterned fabric. The carpet is a Kalogridis Coffee Cut pile with custom accents. Cabinetry is Walnut Burl wood veneer Polished Gold hardware.
Cabin Configuration
Refreshed in 2009 with new window reveal material, carpet and leather work.
The interior is overall Beige / Brown. The fireblocked passenger seats are covered in Desert colored classic Townsend Leather. Window reveals are in Beige textured fabric with the lower sidewalls in Brown patterned fabric. The carpet is a Kalogridis Coffee Cut pile with custom accents. Cabinetry is Walnut Burl wood veneer Polished Gold hardware.
Avionics
PRIMARY AVIONICS:
• Primus 2000 Dual Digital Autopilot/Flight Director EICAS System Five Tube (8” X 7”) Display System with dual ADCs.
• Integrated Primus II Radios with dual 8.33khz. Comms, dual Navs, dual ADF, dual DME, and dual Mode S Enhanced Transponders.
ADDITIONAL AVIONICS:
• Honeywell FMZ-2000 Dual FMS
• Honeywell TCAS II
• Dual KHF 950 Comm
• AlliedSignal EGPWS with windshear
• Aircell Axxess Phone System
• Global AFIS
• Coltech CSD 714 Selcal
• Honeywell Radio Altimeter
• Sextant Three Frequency ELT
• Primus 880 Color Weather Radar
• Fairchild A200S Cockpit Voice Recorder
• Provisions for dual EFB’s
Powerplant
The aircraft is powered by two Allison AE3007C turbofan engines installed on the rear fuselage. The AE3007C features two spools with a 14-stage axial flow compressor, two-stage high pressure turbine and a three-stage low pressure turbine.
The AE3007C incorporates dual channel Full Authority Digital Electronic Controls (FADEC). The engine is a modular design and features six large access panels for Line Replacement Unit (LRU) maintenance and multiple borescope inspection ports.
The engine has a bypass ratio of 5.1 and is rated at a static, sea level takeoff thrust of 6,442 pounds to 86 degrees Fahrenheit.
An APU is incorporated for engine start and other benefits, and is certified for in-flight use. The APU is located in the tailcone stinger for ease of maintenance.
Target-type thrust reversers compatible with the engine nacelles and powerplants are included.
Installed Equipment
RVSM, 110 V Outlets in Cabin and Cockpit, AOA Indexer, Airshow Genesys system, Dual DVD Entertainment System, Tail Logo Flood Lights, Dual Nickel-Cadmium Batteries, Fresh AH Phase Inspection, Aileron Regearing SB Completed.
