Entered into service July 1999

 One UK Fortune 100 owner from new

Total Time : 5912.8 hrs

Engines : (2) Turbomeca Arriel 2S1 Engines.

#1 SN: 20087 Hours : 4137.8 Cycles: 3883 Cycles: 819

#2 SN: 20596 Hours : 505.4   Cycles: 3404 Cycles: 782

Engines are covered by the Turbomeca Power by The Hour Support Programme

Transmissions covered by Sikorsky Total Assurance Plan (TAP)

Maintenance Tracking by AVISA

Weights - Max Takeoff : 11,700 Lbs Empty : 8239 Lbs

INTERIOR DESCRIPTION

(Original Interior 1999 by Sikorsky, West Palm Beach)

This aircraft features a Deluxe VIP “Cocoon” 5/6 passenger

Interior: featuring two aft facing swivelling captain’s chairs

with forward facing three place divan (belted for four).

Aft facing central refreshment centre finished in light

mahogany veneer. The passenger seats are finished medium

grey fabric with tan leather armrests with contrasting sidewalls,

headlining and carpet.

EXTERIOR DESCRIPTION

(Original Paint 1999 by Sikorsky, West Palm Beach )

Repainted 2007 Overall JET-GLO White with Blue and Red accent lines.

AVIONICS

• EFIS: Honeywell EDZ 756
• AHRS: LITEF LCR-92S
• Gull Integrated Instrument Display System
• Communications: (2) Rockwell/Collins VHF-22A VHF Comm
• Radios & (2) Rockwell/Collins
• RTU-4200 RadioTuning Units (RTU’s)
• Navigation: (2) Rockwell/Collins VIR-32 VHF Nav Radios
• Flight Control System / Autopilot: (2) Honeywell SPZ 7600
• Flight Director
• Radar: RDR 2100 Color Weather Radar System
• Transponder: (2) Rockwell/Collins TDR-94 Mode S
• Transponder w/ Diversity
• Automatic Direction Finder: Rockwell/Collins ADF-462 ADF
• Distance Measuring Equipment: (2) Rockwell/Collins
• DME-42 DME
• Radio Altimeter: (2) Honeywell Dual AA-300 Radio
• Altimeter System
• Air Data Computer: (2) Penny & Giles Air Data Computers
• Global Positioning System: Universal UNS-1D FMS
• Flight Management System: Universal UNS-1D FMS
• Traffic Collision Avoidance System: Bendix CAS-66A TCAS I
• Emergency Locator Transmitter System:
• Cockpit Voice Recorder: Universal CVR 30A with ULB Cockpit
• Voice Recorder
• Aircraft status as of October 13, 2009.
• Airframe hours 5917
• Aircraft is Available for Immediate Inspection. Subject to
• Verification Upon Inspection and Withdrawal from the Market.

ADDITIONAL AVIONICS

• Dual Static Inverter AC power System
• Euroavionics Moving Map System
• FZ-706 Digital Flight Control Computer
• AL300 Alt Pre-select
• Honeywell Airsat 1 Satellite Communication
• Standby Attitude Indicator
• Honeywell LP-860 Lightning Sensor System
• Underwater Acoustic Beacon
• Aerosonic Standby Airspeed Indicator
• Allied Signal IU-2023b Graphics Unit Computer with CC2024D Checklist Control Unit
• Airdata Accessory Unit
• Racal V694 Automatic Voice Advisory Device
• Emergency Load Shed Switch

ADDITIONAL INSTALLED EQUIPMENT

• Equipped with Emergency Floatation System
• Upper and Lower Anti-collision Light System
• Retractable Search Light System
• Hella High Intensity Strobe Light System
• Gooseneck Map Lights
• Bose Headsets/Cabin Call/Cabin 6 Place Intercom System
• Four Door Speakers
• Loudhailer System
• Left Hand(AC), Right Hand(DC) Landing Light Assembly
• Pilot / Co-Pilot electric door locks

ADDITIONAL INSTALLED EQUIPMENT

• Electric cabin door locks
• Left and Right Cabin Retractable Boarding Steps
• C-4 Environmental Cabin System
• Cabin Overhead Lateral Absorber
• Long Nose Radome