2016 Leonardo AW109SP GrandNew

Power plant and fuel system
- Two Pratt & Whitney Canada PW207C turbo-shaft engines
- Two independent electronic control systems (FADEC) with normal emergency and training operation modes and auto-start
- Engine mounted fuel pump and filter assembly
- Engine mounted oil pump and filter assembly
- Engine mounted fuel control and governor
- Lubrication and cooling system
- Engine oil chip detectors (2)
- Engine control panel
- Two independent fuel systems with cross-feeding valve and control panel
- 3-cell crash-resistant fuel system (575 – 152 USgal)
- Submerged fuel boost pump (2 each engine)
- Airframe mounted easy access fuel filter
- RH refuelling point
- Ground fuel drains

Transmission drive system and hydraulic system
- 960 shp for takeoff and 900 shp continuous operation main transmission
- Three-stage transmission
- Free wheeling units (2)
- Dual independent, redundant hydraulic systems
- Transmission mounted hydraulic pumps (2) with separate reservoir
- Ripple dampers (2)
- Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
- Transmission oil chip detectors (2)
- Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
- Transmission cooling and lubrication system
- Transmission shafts

Flight/navigation instruments
- Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
- Radio Management System (RMS) RTU-4210 Collins (1)
- VHF/AM VHF-4000E
- VOR/ILS NAV-4500 Collins
- Transponder (Mode S) TDR-94 Collins
- Attitude Heading Reference System (AHRS) (1) with one dual AHRS control panel
- Air Data Unit (ADU) (1)
- Digital Audio Control System (DACS) COBHAM with one cockpit panel
- Electronic clock (1)
- Magnetic compass indicator (1)
- Magnetic sensor unit
- Pitot tube right/left

Instrumentation (on IDS display)
- LCD Integrated Display System (IDS)
- Dual gas generator speed indicator (N1%)
- Dual turbine outlet temperature indicator (TOT°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) 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)
- Two utility hydraulic system pressure indicator (PSI)
- Outside air temperature indicators (°C)
- Two AC voltmeters (VAC)
- Two DC voltmeters (VDC)
- Two DC ammeters (Amp)

Warning/Caution Advisory and Maintenance System
- Master warning lights (2)
- Master caution lights (2)
- Warning, caution and advisory message (on IDS display)
- Aural warning generator system
- Engine fire detection system
- Exceedance recorder system (on IDS display)
- Warning horn (cabin)

Exterior finishing
- Finishing in accordance with manufacturer specification (NTA 893 A)
- Primer exterior painting

- 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 retention straps)