2013 Leonardo AW109SP GrandNew

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
• Internal 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 Collins
• DME 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 clock
• Second 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