2007 AGUSTA A109

2007

AGUSTA

A109

Used

Price: Open to Offers Signed LOI, subject to a pre-purchase inspection, with fully refundable deposit in escrow, will secure. Basic aircraft with cabin passengers sliding doors, equipped with P&W207C engines. Open to Offers.

247.3

Aluminium alloy and bonded panel fuselage Semimonocoque aluminium alloy tail boom Two hinged jettisonable wide crew doors (on both sides) Two sliding passenger doors on both sides, 1.4 m opening with jettisonable windows Acrylic windshield & side windows Acrylic overhead windows Quick removable tail rotor drive shaft cover Three wheel retractable landing gears Separate baggage compartment with hinged door Jacking and hoisting points Removable fairing & cowlings, for complete accessibility to the controls & drive comps Swivelling front wheel with tow bar attachment Quick opening hinged inspection doors to allow visual check of engine oil levels and maintenance inspection points Grounding points Rotors & Controls: Fully articulated corrosion-protected titanium main rotor hub with 4 composite grips, 4 elastomeric bearings, 4 individually interchangeable composite blades with swept tips & dampers Two composite tail rotor blades semi-rigid delta hinged type individually interchangeable Cyclic and collective controls powered by two separate hydraulic systems Hydraulically powered anti-torque TR control system Adjustable friction devices on cyclic and collective system Force trim and artificial feel system Adjustable directional control pedals Dynamic main rotor blade flapping lock mechanism

Two Pratt & Whitney PW207C turboshaft engines Two independent electronic control systems (FADEC) with normal emergency and training operation modes and autostart Engine mounted Fuel Management unit fuel pump and filter assembly Engine mounted oil pump and filter assembly Lubrication and cooling system Engine oil chip detectors (one per engine) Engine control panel Two independent fuel systems with corss feeding valve and control panel 3 cell crash resistant fuel systems Submerged fuel boost pump Airframe mounted easy access fuel filter RH refueling point Locking fuel cap Ground fuel drains Transmission Drive System: 960 shp for take off and 900 shp continuous operation main transmission with two direct drive engine inputs Three stage transmission Two free wheeling units Two transmission mounted hydraulic pumps with separate reservoir Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter Two transmission oil chip detectors Single stage bevel gear TR 90° gear box including oil level sigh glass and hcip detector Transmission cooling and lubrication system Transmission shafts Electrical System: 24 volt DC 27 Ah nickel cadmium battery with temperature probe Two 160 A self cooled starter generators Two voltage regulators Battery relay Two interconnecting bus relay External power relay Distribution buses External power receptacle Two DC ammeters (on IDS Display) Two DC voltmeters (on IDS Display) Position lights Two 150 W taxing lights Two 250 W landing lights Two utility lights Two anti collision lights Instrument lights with dimming switch Radio master switch Propulsion and Hydraulic: Dual torque meter indicator Triple tachometer (one for rotor and two for Nf)

IFR Avionic Package: GARMIN – BENDIX/KING Pilot navigation instruments (LCD EADI and EHSI, stand-by ADI) Gyrocompass C14 Honeywell Vertical gyro #1 46060-11 Flightline System Vertical gyro #2 VG-208 JET Electronics 3-axis duplex AFCS SP711 Honeywell ADF KR-87 Bendix/King Transponder (mode S) KT-73 Bendix/King VHF#1 Com/Nav/GPS GNS 530 Garmin VHF #2 Com/Nav/GPS GNS 430 Garmin Pilot ICS (including pilot/copilot control panel, model controller, audio cabin control) DME KDM706A Bendix King Marker Beacon KMR675 Bendix/King AC Power supply system (two inverters) Additional Installed Avionic Equipment: Copilot flight/navigation instruments (LCD EADI & EHSI barometric altimeter airspeed indicator VSI) Flight director FZ 702 Honeywell with autotrim Radio altimeter AA 300 Honeywell ELT C406-2HM Artex Moving map KMD 550 Bendix King Radio master switch with ground function EFIS pilot/copilot in command switch Flight Instruments - Pilot: Airspeed indicator Instantaneous vertical speed indicator Barometric encoding altimeter Magnetic compass indicator Clock 8 days and elapsed time LC integrated display system Instruments (on IDS Display): Transmission oil temperature and pressure indicator Two engine oil temperature and pressure indicator Two fuel pressure indicator Two fuel quantity indicator Dual gas generator tachometer Indicator Dual turbine outlet temperature indicator Two flight controls hydraulic system pressure indicators Two utility hydraulic system pressure indicators

Standard Additional Equipment: Pilot & copilot headsets Pilot & copilot shoulder harness with inertia reel Baggage compartment light Crew open door actuators Quick disconnecting chip detectors Portable fire extinguisher Structural provision for utility equipment (emergency floats, rescue hoist, cargo hook, weather radar, engine fire extinguisher, flight director, AFCS) Fuel drain electrical valves Tail boom strake First aid kit Airframe hour meter Installed Utility/COMF Equipment: Dual Control Rotor Brake 450 W Retractable / Rotating landing light Pilot & copilot windshield wipers with wiper switch on cyclic grip Engine compartment fire extinguishers Baggage compartment extension (to 1.9 m) Miscl. Equipment: Air intake / exhaust covers Pitot tubes covers Tie-down fittings provisions Rotorcraft Flight Manual and technical publications 213 USG crash resistant fuel system Particle separator – engine air induction system Weather radar displayed in EFIS Baggage compartment extension (2.3 m) Warning Advisory and Main System: Master Warning lights Master caution lights Warning caution advisory (on IDS display) Engine fire detection system Aural warning generator system Exceedance recorder system (on IDS display)

Finishing in accordance with manufacturer specification 109-05-03 Primer exterior painting

Air conditioning ECU Garret Primer finished cabin walls Passive vibration absorber Interior Completion: VIP Interior Paulstra soundproofing Leatherette covered or painted liners 3 seat aft facing central bench with see-through foldable armrest 3 seat fwd facing crash resistant aft bench with armrest All seats crash resistant VIP model covered with leather 4 point shoulder harness with inertia reels & safety belts Advisory reading lights Leather bellows on flight controls Floor carpeting Cabin double layer acrylic windows 6 Active Noise Reduction ANR headset Customised pax cabin finishing Carpeting protection Seat covers Pilot console tray Pilot & co-pilot aft holders Suede covered liners Chest of 3 drawers Interior Arrangement: Two individual crash-resistant pilot seats fore & aft adjustable, with lap belts. Aluminium alloy honeycomb reinforced floor with anti-skid finishing Ventilation ram air inlets Anti reflection instrument panel Primer finished cabin walls