Exterior
Overall snow white with ocean blue metallic, strawberry pearl and titanium metallic stripes.
Interior
An overall elegant beige interior. The fireblocked passenger seats are covered in pumice Townsend leather. Window reveals are covered in crème textured fabric with the lower sidewalls in a beige leather. The carpet is sand and pebble cut pile. The cabinetry is finished in walnut burl high gloss wood veneer with brushed aluminum hardware.
Cabin Configuration
Six passenger seats are arranged in a center club configuration with a belted flushing toilet in the lavatory. Cabin furnishings consist of RH refreshment center, an optional LH storage cabinet with 8.4” AvVisor Plus display and a RH navigation chart case. Work surfaces include dual executive and slimline tables. Other options include 110V outlets and an Aircell phone system.
Avionics
PRIMARY AVIONICS:
• Collins Proline 21 Integrated Flight Director and Autopilot with optional 3-tube 8x10 inch EFIS.
• Collins ProLine 21 CNS Radios with dual COM, dual NAV, single DME, dual Radio Tuning Units (RTUs) and dual TDR-94D Mode S Diversity Transponders.
ADDITIONAL AVIONICS:
• Collins FMS-3000 with GPS
• Collins HF-9000 (Provisions Only)
• Honeywell Mark VIII EGPWS
• FA 2100 CVR
• Collins WXR-800 Radar
• Garmin GPS-500
• TCAS-4000 (TCAS II)
• Integrated Pulselight System
• Artex C406-N ELT
• AvVisor Plus Display
Powerplant
Two Williams FJ44-3A turbofan engines are installed, one on each side of the rear fuselage in easily accessible nacelles. This engine is a medium bypass, twin-spool design with 5 compression stages and 3 turbine stages and produces 2,8200 pounds (12.54 kN) of takeoff thrust at sea level, static conditions, flat rated up to 79° F (26°C).
Dual channel Full Authority Digital Engine Controls (FADECs) provide automation and efficiency in engine management. Detents in the throttle quadrant for takeoff (TO), maximum continuous (MCT), high speed cruise (CRU) give pilots the optimal power settings for each phase of flight based on ambient conditions. The system also provides time-limited dispatch (TLD), diagnostics, and engine synchronization. Electrical power for the FADECs comes from engine driven permanent magnet alternators (PMAs) rectified to DC. There are two PMAs mounted to each engine. In the event that both PMAs fail on one engine, the FADEC on that side will draw from main DC power.
The FJ44-3A engine incorporates a modular design and multiple borescope ports for easier maintenance and inspections. Engine overhaul is required at 4,000 hour intervals. 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 supplied.
Installed Equipment
RVSM, PSU Indirect Lighting, XM Broadcast Weather, Voice Annunciator, Jeppesen Electronic Charts, Tail Flood Lights, Pilot’s AOA Indexer, Cockpit Speaker Mute Switch, HectoPascal/Inch Switch, 50 Cubic Foot Oxygen, B/E Aerospace Crew Oxygen Masks, Monorail Sunvisors, Avionics Ground Power Switch, Airstair Cabin Entry Step.
