2012 Agusta / Leonardo AW109SP Grand New

Notes/Highlights

Single Pilot IFR

LPV capable

4-axis dual duplex digital AFCS with integrated Flight Director

Moving map EURONAV V with 8.4” display

VIP interior completion 5 seats

Air conditioning ECS (Environment Control System)

Twin engine PW207C

Annual inspection done September

Interior

• Air conditioning ECS (Environment Control System)

• Primer finished cabin walls

• VIP interior completion 5 seats, 5 ANR headsets

• Sheepskin Covers (crew seats)

• Domelight cockpit

• Set of 3 Drawers

Exterior Painting

• Standard colour scheme from Company paint selection, solid colour

Avionics

• 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) 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)

• Electronic Standby Instrument System (ESIS)

• Traffic Avoidance System TAS-620 Avydine (presented on EFIS)

• Weather Radar (displayed on EFIS)

• Reversionary Control Panel (RCP)

• EFIS pilot/co-pilot naviagation synchronization switch (FMS data)

• VOR/ILS/ADF NAV-4000 Collins

• DME DME-4000 Collins

• Radio altimeter ALT-4000 Collins

• Pilot GPS/SBAS Chelton interfaced to EFIS/FMS

• Co-pilot GPS/SBAS Chelton interfaced to EFIS/FMS

• 4-axis dual duplex digital AFCS with integrated Flight Director

• ELT C406-N HM Artex (with Navigation Interface Module embedded)

• Moving map EURONAV V with 8.4” Display

• Enhanced Vision System (EVS) EVS-1500 Max-Viz

• Second Radio Management System (RMS) RTU-4210 Collins

• Second VHF/AM VHF-4000E Collins

• Digital Audio Control System (DACS) NAT additional cockpit panel

• Second electronic clock

• Second magnetic compass indicator

• Second Altitude Heading Reference System (AHRS)

• Second Air Data unit (ADU)

Optional equipment

• Crash-resistant pilot and co-pilot seat, fore and aft adjustable, with lap belts and headrest

• Shoulder harness with inertial reels (pilot and co-pilot)

• Active Noise Reduction (ANR) headsets (pilot and co- pilot)

• Crew open door actuators

• Reinforced windshields

• Windshield wipers (pilot and co-pilot)

• Retractable/rotating landing light (nose mounted)

• Electrically Operated Passenger Step (LH & RH)

• Engine compartment fire extinguishers (Qty 2)

• Engine washing kit provisions

• Rotor brake

• Emergency floats (Fixed provision parts)

• 5 cells crash-resistant fuel system (213 US gal) with fuel drain electrical valves

• Baggage compartment extension (2.3 m)

• Baggage compartment lights

• Tailboom strake

• Fuel cap with key lock

• Pulsed chip detectors (in lieu of quick disconnecting chip detectors)

• Strobe Lights on Horizontal Stabilizers

• Map Lights for Pilot/Co-Pilot

• Dual controls

• Pilot Multipurpose Holder

• Pilot/Co-Pilot Console Tray

• Airframe Hourmeter

Additional

• Blade Tie Downs

• Engine Air Intak Covers

• Exhaust Covers

• Towing bar