Exterior
New paint in October 2007. Overall Snow White with Black Metallic, Tibetan Gold Metallic and Las Vegas Gold stripes.
Interior
Refurbished in November 2007. The interior is overall Beige / Brown. The fireblocked passenger seats are covered in Desert colored classic Townsend Leather. Window reveals are Rose Gold Lavie fabric with the lower sidewalls in Brown patterned fabric. The carpet is Kalogridis Coffee velour. Cabinetry is Walnut Burl wood veneer Polished Gold hardware.
Cabin Configuration
Eight passenger seats are arranged in a double club configuration. The cabin includes four executive tables, a L/H forward closet with a VCR Player and CD Player, and a R/H forward refreshment center. The aft lavatory contains a vanity cabinet, an externally serviceable flushing toilet, and an Aft Closet. 110V outlets are located in the cabin and cockpit.
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 (8.33) 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 HF Radios
• Honeywell EGPWS with windshear
• Aircell ST-3100 Phone System
• Global AFIS
• Coltech CSD 714 Selcal
• Honeywell Radio Altimeter
• Litton Three Frequency ELT
• Primus 880 Color Weather Radar
• Fairchild A200S Cockpit Voice Recorder
• A.O.A. Computer
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, 76 Cubic Foot Oxygen, Pulse Lights, Thrust Reversers, 110 V Outlets in Cabin and Cockpit, Airshow Genesys Cabin Information Display, Aileron Regearing Modification, Glareshield Supplemental Lighting, VCR and CD Players, Tail Logo Flood Lights, Dual Nickel-Cadmium Batteries.
