2013 Leonardo AW109 Grand New

S/N: 22297 | C-FKAM

Total Hours
720 hours since new

Engines
Pratt & Whitney PW 207C

# TSN
Engine 1 720
Engine 2 720

Highlights

  • 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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Details

Standard Equipment

  • 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)

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