2016 AGUSTA AW119 Koala SOLD

Airframe • Aluminium alloy and bonded panel fuselage • Semi-monocoque aluminium alloy tail boom • New reinforced skid type landing gear • Two hinged jettisonable crew doors (LH RH) • Two sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows • Passenger short foot step (LH RH) • Acrylic windshield and side windows • Overhead cockpit transparent windows • Lower cockpit transparent windows • Removable fibreglass tail rotor gearbox fairing • Quick removable tail rotor drive shaft cover • Separate baggage compartment with hinged door • Three jacking points • Removable fairing and cowlings, for complete accessibility to the controls and drive components • Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points • Grounding points Rotors and Controls • Titanium main rotor hub, corrosion protected, fully articulated with four composite grips, four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampers • Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable • Cyclic and collective controls powered by two hydraulic systems • Hydraulically powered anti-torque system • Adjustable friction devices on cyclic and collective system • Force trim and artificial feel system • Adjustable directional control pedals • Flapping and droop restraint mechanism Power Plant and Fuel System • Pratt Whitney Canada PT6B-37A turbo-shaft engine • Engine mounted fuel pump and filter assembly • Engine mounted oil pump and filter assembly • Engine mounted fuel control and governor • Electronic Engine Control (EEC) • Lubrication and cooling system • Engine oil chip detector (1) • Engine mounted fuel heater • Fuel system control panel • 3-cell fuel system (605 l – 160 US gal) • Submerged fuel pumps (2 boost and 1 transfer pump) • RH refuelling point Transmission / Drive System and Hydraulic System • 917 shp for take-off and 900 shp continuous operation main transmission • Two-stage transmission • Transmission mounted hydraulic pumps (2) with separate reservoir • 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 Electrical System • 28 V DC 22 Ah nickel-cadmium battery with temperature probe • 200 A self-cooled starter generator • Voltage regulator • Battery relay • Interconnecting bus relay • External power relay • Distribution buses (2) • External power receptacle • Position lights (NVG compatible) • 250 W landing lights (2) • Anti-collision lights (2) (NVG compatible) • Cockpit utility lights (2) (NVG compatible) • Instrument lights • Radio master switch Avionic Package Depending on both contractual delivery date and Country of destination, the AW119Kx helicopter could be delivered with EASA/FAA Type Certification or could be equipped with Garmin G1000HTM approved as FAA STC. The latter does not include the magnetic compass indicator. • Garmin G1000HTM Integrated Flight Deck system comprising: – Two GDU-1040 10.4” display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:  Radio tuning controls  Flight Management System (FMS)  Synthetic Vision System  Helicopter Terrain Awareness and Warning System (HTAWS) – Two GEA-71H Aircraft Interface Unit – Two GSC-46 Signal Conditioners – GRS-77H AHRS – GDC-74H Air Data Computer (ADC) – Two GIA-63H Integrated Avionics Units (IAU) comprising:  COM 1 2  NAV 1 2  GPS 1 2  Aural Alert Generator  ADF interface  DME tuning interface – GTX-33H Mode-S Transponder with Extended Squitter (ES) capability • Radar Altimeter RA-4500 FreeFlight Systems • Digital Audio Control System (DACS) COBHAM with two cockpit panels • Magnetic Compass indicator • L3 Avionics System ESI-2000 Electronic Standby Indicator • Engine Hour meter Systems Data (on PFD/MFD) • Inter turbine gas temperature indicator (ITT°C) • Engine torque indicator (TQ%) • Compressor speed indicator (N1%) • Turbine speed indicator (N2%) • Rotor speed indicator (NR%) • Transmission oil pressure (PSI) and temperature (°C) indicator (on MFD) • Engine oil pressure (PSI) and temperature (°C) indicator (on MFD) • Fuel pressure (PSI) (on MFD) and fuel quantity (kg) indicator (on PFD/MFD) • Two hydraulic pressure system indicators (PSI) (on MFD) • Outside air temperature indicator (°C) (on PFD) • DC voltmeter (VDC) (on MFD) • DC ammeter (Amp) (on MFD) Central Warning System (CWS) • Master warning lights • Master caution lights • Warning, caution and advisory messages on PFD display • Aural alerts from IAU 1 2 Interior Arrangement • Pilot and co-pilot seats, fore and aft adjustable, with lap belts and headrests • Alumi