2013 Leonardo AW109SP GrandNew for sale, England, United Kingdom

— Dual / Single IFR package
— Pilot Flight/Navigation EFIS (2 displays)w/embedded FMS,
— Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp)
— Co-pilot flight/navigation EFIS (2 displays) w/ embedded FMS,
— Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp)
— EFIS pilot / co-pilot navigation synchronization switch (FMS data)
— Electronic standby instrument system (ESIS)
— Second radio management system (RMS) RTU-4210 Collins
— Radio manager system (RMS) RTU-4210 Collins
— VHF/am VHF-4000e (2 unit s )
— VOR/ILS Nav-4500 Collins
— VOR/ILS/ADF/Nav-4000
— Collins
• 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) cobham additional cockpit panel
— 4-axis dual duplex digital AFCS with integrated Flight Director
— Second electronic clock
— Second magnetic compass indicator
— ELT C406-N HM Artex (w/ navigation interface module embedded)
— 8.4 Cockpit central Display
— Transponder (mode S) TRD-94 Collins
— Attitude heading reference system (AHRS) w/ one dual AHRS control panel
— Air data unit (ADU)
— Digital audio control system (DACS) Cobham w/ additional cockpit panel
— Magnetic sensor unit
— LCD integrated display system ( IDS)
— Dual gas generator speed indicator (N1%)
— Dual turbine out let temperature indicator ( ̊c)
— Dual torque meter indicator (TQ%)
— Dual power turbine speed indicator (N2%)
— Rotor speed indicator (NR%)
— Transmission oil pressure (psi ) and temperature ( ̊c) indicator
— Two engine oil pressure (psi i)and temperature ( ̊c)indicators
— Two fuel pressure indicators (psi )
— Two fuel quantity indicators (kg)
— Two fuel flow indicators(kg/ hr)
— Two flight controls hydraulic system pressure indicators (psi )
— Out side air temperature indicator ( ̊c)
— Two AC voltmeters
— Two DC voltmeters

— VIP/Corporate interior – 5 places (inc inter seat console)
— All seat s crash-resistant covered with leather
— 4-point Shoulder Harness with Inertia reels and Safety Belts for all seats
— Super Silent Soundproofing
— Intercommunication system for passengers
— Headset BOSE ANR type (qty 5)
— Cabin loudspeakers (qty 2)
— Air conditioning ECS (Environment Control System)
— Reading lights, emergency lights, floor courtesy lights
— Upper and Lower Air Vents
— Floor Carpeting
— Seat Covers

— Emergency float s provisions (Fixed Parts Only – No Float Bags )
— 213 us gal crash-resistant fuel system ( in lieu of 152 US gal )
— Baggage compartment extension (2.3m)
— Engine compartment fire extinguisher (qty 2)
— Fuel Cap with Key-Lock
— Pulsed Chip Detectors
— Rotor Brake
— Retractable/Rotating Landing Light (nose mounted)
— Retractable/Rotating Landing Light (nose mounted)
— Ground Equipment
— Air Intake / Exhaust Covers
• Tow bar and chocks
— Pitot covers
— Rotorcraft Flight Manual (RFM) and Technical Publications
— Tie-downs