2008-AW109S Grand For Sale

Agusta AW 109S Grand

For Sale

US$ POA

Year: 2008 | TTAF: 385

Highly maintained helicopter in excellent condition.

 

AGUSTA WESTLAND GRAND STANDARD SINGLE/DUAL PILOT IFR CONFIGURATION (EASA/FAA)

1.1 BASIC AIRCRAFT

  • Basic aircraft with cabin passengers sliding coors, equipped with P&W207C engines.

1.2 STANDARD ADDITIONAL EQUIPMENT

  • Pilot and copilot headsets
  • Pilot and 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

1.3 SINGLE PILOT IFR/FAA AVIONINC 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 A F C S SP711 Honeywell
  • ADF KR-87 Bendix/King
  • Transponder (mode S) KT-73 Bendix/King
  • VHF#1 COM/NAV/GPS GNS530 Garmin
  • VHF #2 COM/NAV/GPS GNS430 Garmin M
  • DME KDM706A Bendix/KineflT,
  • Marker beacon KMR675 Bendix/King
  • Pilot ICS (including pilot/copilot control panel, mode controller, audio cabin control)
  • AC power supply system (two inverters)

1.4 ADDITIONAL INSTALLED AVIONIC EQUIPMENT

  • Copilot flight/navigation instruments (LCD EADI and EHSI, barometric altimeter, airspeed indicator, VSI)
  • Flight director with autotrim FZ 702 Honeywell
  • 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

1.5 INSTALLED UTILITY/COMFORT EQUIPMENT

  • Dual control
  • Rotor brake
  • 450 W Retractable/Rotating landing light
  • Pilot and copilot windshield wipers with wiper switch on cyclic grip
  • Engine compartment fire extinguishers
  • Baggage compartment extension (to 1.9 m)

1.6 INTERIOR

  • Air conditioning ECU Garret
  • Primer finished cabin walls
  • Passive vibration absorber

1.7 PAINTING

  • Single coior painting scheme, solid colors, series 300

1.8 MISCELLANEOUS EQUIPMENT

  • Air intake/exhaust covers
  • Ptot tubes covers
  • Tie-down fittings provisions
  • Rotcrcraft Flight Manual and technical publications
  • Ground tools kit (including tow bar, lifting tool, wheel chocks)

2. AIRFRAME

  • 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) 1.40 m opening with jettisonable windows
  • Acrylic windshield and 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 and cowlings, for complete accessibility to the controls and drive components
  • Swiveling 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

3. ROTORS AND CONTROLS

  • Fully articulated corrosion-protected titanium main rotor hub with 4 composite grips, 4 elastomeric bearings, 4 individually interchangeable composite blades with swept tips and dampers
  • Two composite tail rotor blades semi-rigid delta hinged type, individually interchangeable
  • Cyclic and collective controls powered by two separate-redundant hydraulic systems
  • Hydraulically powered anti-torque T/R 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 mechanic

4. POWER PLANT AND FUEL SYSTEM

  • Two Pratt & Whitney PW207C turboshaft engines
  • Two independent electronic control systems (FADEC) with normal' emergency and training operation modes and auto-start
  • Engine-mounted Fuel Management Unit (FMU), 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 cross-feeding valve and control panel 3-ceil crash-resistant fuel system (460 kg - 152 USG) Submerged fuel boost pump (one per system)
  • Airframe mounted easy access fuel filter
  • RH refueling point
  • Locking fuel cap
  • Ground fuel drains

5. 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 T/R 90° gear box including oil level sight glass and chip detector
  • Transmission cooling and lubrication system
  • Transmission shafts (engines to transmission to tail rotor)

6. ELECTRICAL SYSTEM

  • 24 volt DC 27 Ah nickel cadmium batter/ with temperature probe
  • Two 160 A self cooled starter generators
  • Two voltage regulators Battery relay
  • Two interconnecting bus relay
  • External power relay
  • Distribution buses (1 battery bus. 2 essential buses. 2 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

7. 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 (IDS)

8. PROPULSION AND HYDRAULIC INSTRUMENT (ON IDS DISPLAY)

  • Dual torque meter indicator
  • Triple tachometer (one for the rotor and two for Nf)
  • Transmission oil temperature and pressure indicator
  • Two engine oil temperature and pressure indicator
  • Two fuei 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

9. WARNING/CAUTION ADVISORY AND MAINTENANCE 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)

10. INTERIOR ARRANGEMENT

  • Two individual crash-resistant pilot seats fore and 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

11. EXTERIOR FINISHING

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

12. OPTIONAL EQUIPMENT

  • 1. Executive Interior - 6 places
    • a Silent soundproofing
    • b. Leatherette covered liners
    • c. All seats crash-resistant covered with fabric
    • d. 3 aft facing seats (central bench)
    • e. 3 fwd facing seats (aft bench)
    • f. 4-point shoulder harness with inertia! reels and safety belts for all passenger seats
    • g. Reading lights, advisory lights, floor courtesy lights
    • h. Cabin loudspeakers
    • i. Floor carpeting
    • j. Standard finishing
  • 2. 213 USG crash-resistant fuel system
  • 3. Customized painting scheme, metallic colors
  • 4. Reinforced pilot and co-pilot windshield
  • 5. Cabin double layer acrylic windows
  • 6. Pilot and co-pilot multipurpose holders
  • 7. Pilot and co-pilot console tray including 12 V outlet
  • 8. Pulsed chip detectors
  • 9. Baggage compartment extension (2,3 m)
  • 10. High-intensity strobe lights on horizontal stabilisers
  • 11. Fuel cap with key-lock
  • 12. Super Silent soundproofing (in Lieu of Silent Sound-proofing)
  • 13. Electrically operated passenger step (RH)
  • 14. Passenger seats with leather covering

 

 


 SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION HELICOPTER IS OFFERED SUBJECT TO PRIOR SALE OR WITHDRAWAL FROM THE MARKET AIRCRAFT WILL CONTINUE TO REMAIN IN FLIGHT SERVICE UNTIL FORMAL DEPOSIT IS PLACED.
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