- Aerolite EMS interior
- Hoist, Aux Fuel
- Cockpit Central Display, Weather Radar
- Multi-band Airborne FM transceiver
- Fixed parts CV-FDR, SX16 searchlight, loudspeaker, EVS
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Total Hours
878 hours since new
Engines
Pratt & Whitney PW207C
Engine |
TSN |
|
Engine 1 |
878 |
|
Engine 2 |
878 |
|
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- Airframe hourmeter
- Baggage compartment extension (1.9 m)
- Baggage compartment lights
- Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrest
- Crew open door actuators
- First aid kit
- Fuel drain electrical valves
- Internai structural provisions for utility equipment
- Portable fire extinguisher
- Shoulder harness with inertial reels (pilot and co-pilot)
- Tail boom strake
Additional Equipment
- Active Noise Reduction (ANR) headsets (pilot and co-pilot)
- Engine compartment fire extinguishers (Qty 2)
- Fuel cap with key-lock
- Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
- Reinforced windshields
- Retractable/rotating landing light (nose mounted)
- Rotor brakeWindshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
Misc/ground equipment
- Air intake/exhaust covers
- Ground tools kit (including tow bar, lifting tool, wheel chocks)
- Pitot tubes covers
- Rotorcraft Flight Manual (RFM) and technical publications
- Tie-down fittings (main rotor and tail rotor retention straps)
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Single Pilot Dual Controls IFR avionic package
- Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP) (*) in lieu of basic Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
- Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and Remote Bug Panel (RBP)
- Reversionary Control Panel (RCP)
- EFIS pilot/co-pilot navigation synchronization switch (FMS data)
- Electronic Standby Instrument System (ESIS)
- Second Radio Management System (RMS) RTU-4210 Collins
- Second VHF/AM VHF-4000E Collins
- VORIILS/ADF NAV-4000 CollinsDME DME-4000 Collins
- Radio altimeter ALT-4000 Collins
- Second Attitude Heading Reference System (AHRS)
- Second Air Data Unit (ADU)
- Pilot GPS/SBAS Chelton interfaced to EFIS/FMS
- Co-pilot GPS/SBAS Chelton interfaced to EFIS/FMS
- Digital Audio Control System (DACS) NAT additional cockpit panel4-axis dual duplex digital AFCS with integrated Flight Director
- Second electronic clockSecond magnetic compass indicator
- ELT C406-N HM Artex (with Navigation Interface Module embedded)
- Dual controls
Painting
- Standard colour scheme from Company paint selection, solid colour
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