This 2011 Agusta AW109 SP GrandNew is a well-equipped turbine helicopter currently offered for sale in Switzerland. The aircraft features a single-pilot, dual-control IFR configuration with a comprehensive avionics package, including a Collins VHF-4000E radio, VOR/ILS NAV-4500, Mode S transponder, and an integrated digital audio control system. The VIP-configured cabin benefits from crash-resistant seating and an aluminum honeycomb floor with anti-skid finishing, while the exterior maintains its original manufacturer-applied paint scheme.

Powered by twin Pratt & Whitney Canada PW207C turboshaft engines with FADEC controls, the helicopter delivers 960 shp for takeoff and 900 shp continuous operation through a robust three-stage transmission system. The airframe combines aluminum alloy and composite materials with retractable landing gear, jettisonable crew doors, and quick-access maintenance panels. Notable features include a fully articulated titanium main rotor hub with composite blades, dual redundant hydraulic systems, and a 575-liter crash-resistant fuel system. The aircraft has recently undergone an annual inspection and remains ready for IFR operations with its EFIS display system and comprehensive flight instrumentation.

Avionics

PFD

EFIS - PILOT FLIGHT/NAVIGATION EFIS (1 DISPLAY) WITH SLIP INDICATOR AND REMOTE BUG PANEL (RBP)

Comms

RTU-4210 - RADIO MANAGEMENT SYSTEM (RMS) COLLINS VHF/AM

NAV-4500 - VOR/ILS COLLINS TRANSPONDER (MODE S) COLLINS ATTITUDE HEADING REFERENCE SYSTEM (AHRS) (1) WITH ONE DUAL AHRS CONTROL PANEL

Audio

DACS - DIGITAL AUDIO CONTROL SYSTEM (DACS) NAT WITH ONE COCKPIT PANEL

EMS/EIS

IDS - 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 INDICATORS (PSI) OUTSIDE AIR TEMPERATURE INDICATOR (°C) TWO AC VOLTMETERS (VAC) TWO DC VOLTMETERS (VDC) TWO DC AMMETERS (AMP)

Additional Equipment

Fuel System

3-CELL CRASH-RESISTANT FUEL SYSTEM (575 L –152 USGAL) SUBMERGED FUEL BOOST PUMP (2) AIRFRAME MOUNTED EASY ACCESS FUEL FILTER RH REFUELLING POINT & GROUND FUEL DRAINS

Hydraulic System

DUAL INDEPENDENT, REDUNDANT HYDRAULIC SYSTEMS TRANSMISSION MOUNTED HYDRAULIC PUMPS (2) WITH SEPARATE RESERVOIR RIPPLE DAMPERS (2)

Transmission

MAIN TRANSMISSION THREE-STAGE TRANSMISSION FREE WHEELING UNITS (2)

Interior & Exterior

Interior Notes: CRASH-RESISTANT PILOT SEAT, FORE AND AFT ADJUSTABLE, WITH LAP BELTS AND HEADREST ALUMINIUM ALLOY HONEYCOMB REINFORCED FLOOR WITH ANTI-SKID FINISHING VENTILATION RAM AIR INLETS ANTI REFLECTION INSTRUMENT PANEL