Description:

Helicopter Has Had 1 VVIP Owner and Features The Following Equipment

Rear Avionics Compartment
Mast Moment System
Central Panel Display System- CPDS
Rotor Brake
Pilot Window with Sliding Vent
High Visibility Main Rotor Blade
Metro Landing Gear Extensions
Metro Auxiliary landing Light-Cross Tube Mounted
Fuel Management System
Radar Radome (Including Landing Light Relocation)
Reinforced Rear Landing Gear Tube

Airframe:
Total Time 760 Hours
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Avionics/Radios:
Thales Meghas Single System
(2) SMD45 Display - EAD/EHSI
(2) ICP Control Unit
(1) RCU Reconfiguration Control
(2) FCDM Flight Control Display
Display Ventilation for Sextant Displays
GPS/NAV/COM-1 GNS530 - GPS/NAV/COM-2 GNS430
Transponder, Mode S GTX330
Radar Alt KRA405B
Weather Radar RDR 2000
DME Transceiver CDM-451
Audio Panel-Pilot & Copilot AA95
ELT C406-2HM
MFD Display GMX-200
FM Transceiver TFM500/G
Marker Beacon KR21
Honeywell Traffic Avioidance KTA-810
Digital Automatic Flight Control System - (DAFCS)
Pitch/Roll CSAS for IFR included with Autopilot
Sensor Kit, consisting of:
AHRS - Dual APIRS 2101F (SFIM)
Air Data System - Dual ADU 3000
Pelican Rack (4 slot)
Single AC System with Inverter
Copilot Pitot/Static System
Dual Flight Controls
AHRS Free Steering Mode
NVG Compatible Cockpit Layout
RH Instrument Panel Extension - Metro
Center Console
Slant panel
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Additional Equipment:
40 Ah Lead Acid Battery Upgrade
Starter/generator - 2 X 200A, 28VDC
Windshield Wiper System - single blade
Landing & Searchlight, retractable, 200/400W
Wire Strike Protection System
Engine compressor Wash Device
Collective Activated Hourmeter
Tinted Sun Shades for Cockpit Roof Section
Anti-Collision Light - Vertical Fin
Apical Emergency Floats with deployable Life Raft
Supplemental Strobe Lights on Horizontal Stab Fins
Pulse Chip Detectors for Engines, MGB and TRGB
HEEL's Exit Lighting
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Interior:
Dedicated Corporate Interior
Six Passenger Rear Seating
Height-adjustable Pilot & Copilot Seats
Tinted Windows - Cabin
Bleed Air Heating
Metro Air Conditioning System
Leather Interior with Enhanced Sound Proofing
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Inspection Status:
Transition Training for two Pilots - Training conducted at AHI Grand Prairie Texas in S/N 0735.
6 Month/100 Hour Limited Airframe Warranty
Component times match airframe times