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  • Alert Me Name: Agusta AW109E Power
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Agusta AW109E Power
Please Call
  • YEAR
    1997
  • LOCATION
    Europe, England, United Kingdom
  • S/N
    11010
  • REG
    2-SEXY
  • TTAF
    4216

Aircraft Highlights

VIP 1997 AW109 –one previous owner –always hangered –completely refurbished by Leonardo Service Centre
Excellent maintenance records-maintained from new at Leonardo Service Centre
Highest specification six seat VIP interior including set of three under seat drawers
Optional equipment including optional sixth seat can be replaced with a centrearm rest with refrigeration unit and drawers
Weather radar –TAS 497 –baggage compartment extension (2.3m)

AIRFRAME

Total Time Airframe 4216 Hours
Single Pilot IFR (EASA/FAA)
2x Avidyne440 Com/Nav/GPS. (WAAS approved gps for primary nav)
Vertical gyro VG208 (x2)
AvidyneAXP 322 mode S transponder
ICS pilot including:
PS Engineering PMA 7000
Pilot/co-pilot/passenger control with aux music input
AvidyneTAS605A traffics avoidance system w/ ADS-B
Collins DME 42
ADF KR87

Power Plant, Fuel System & Electric Drive System
Two Pratt & Whitney PW206C 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 oil chip detectors (two)
Two independent fuel systems with
cross-feeding valve and control panel
Submerged fuel boost pump (one per system)
Transmission oil chip detectors (two)
Two transmission mounted hydraulic pumps (two) with separate reservoir
Engine-mounted oil pump and filter assembly
Airframe mounted easy access fuel filter
Three cell crash resistant fuel system (152 USG)
Locking fuel cap

Rotors & Controls
Fully articulated corrosion-protected titanium metal main rotor hub, with four composite grips, four elastomeric bearings, four individually interchangeable composite blades, swept tips and dampers
Two composite tail rotor blades semi-rigid delta
hinged type individually changeable
Cyclic and collective controls powered by two separate 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 mechanism

Electrical System
24 V DC 27 Ah nickel cadmium battery with
temperature probe
Two 160 A self-cooled starter generators
Two voltage regulators
Battery relay / external power relay
Two interconnecting bus relays
External power relay
Distribution buses (one battery, two essential, two emergency, two main)
External power receptacle
Two DC ammeters (on IDS display)
Two DC voltmeters (on IDS display)
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


Factory Installed
Co-pilot flight/navigation instruments including:
Barometric altimeter
Air Indicator
VSI
LCD EADI and EHSI
Honeywell radio altimeter
ArtexC406-2HM ELT
Honeywell FZ 702 flight director
Completely refurbished in Nov 2017 with Versace inspired interior
3 forward facing seats in black and white leather
Three aft facing seats with foldable armrest
Three point shoulder harness with inertia reels and safety belts
Black carpet and white ultra leather interior
Leather bellows on flight controls
Cabin double layer acrylic windows
Advisory and reading lights
Paulstrasuper silent soundproofing
BOSE noise cancelling headsets
Recently painted in pearlescent white paint
Weather radar
Emergency float provisions
Extended baggage bay
Fuel cap with key

AIRFRAME:
Aluminiumalloy and bonded panel fuselage
Semi-monocoquealuminium alloy tail boom
Two hinged jettisonablecrew doors (LH and RH)
Two passenger sliding doors with jettisonablewindows (LH and RH) with 1.40m opening
Acrylic windshield and side windows
Acrylic overhead windows
Grounding points
Three wheel retractable landing gear
Seperate baggage compartment and hinged door
Jacking and hoisting points
Removable fairing and cowlings, for complete accessibility to the controls and drive components
Swivelling front wheel provided with tow bar attachment Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points

Rotor brake
450W rotating landing light
Engine compartment fire extinguisher
Windshield wipers (pilot / co-pilot)
Vibration absorber
Air conditioning (Garret ECU)
Dual controls
Engine chip burner
Airframe hourmeter
Wiper switch on cyclic grip
Left and right auxiliary fuel tanks
Air intake exhaust covers
Tie-down fittings provisions
Ground tools kit including lifting tool, tow bar and wheel chocks
Pitot tube covers
Flight manual and technical publications

Agusta AW109E Power

Please Call
  • YEAR
    1997
  • LOCATION
    Europe, England, United Kingdom
  • S/N
    11010
  • REG
    2-SEXY
  • TTAF
    4216
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