2001 Agusta AW109E Power For Sale, United Kingdom

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2001 agusta aw109e power with metallic silver with metallic blue stripes
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Now Sold
Europe, United Kingdom - England
Year
2001
S/N
11111
Reg
G-MIHA
TT
3688 hrs

Aircraft Description

- Fresh EASA C of A, 200hr and Annual
- 90 hours since overhaul on both engines
- Clear of maintenance with no major components due overhaul
- Immaculate condition 
- 6 place cream leather VIP interior

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Volare Aviation Ltd
  • AIRFRAME / ENGINES / APU / WEIGHT / TOTAL TIME / TOTAL LANDING

    TOTAL TIME

    3688 hrs
  • AVIONICS & CONNECTIVITY
    Single pilot IFR Cockpit with Four Rogerson Kratos EFIS Displays
    Single Honeywell SP-711 Three Axis Autopilot
    Single Honeywell FZ-702 Flight Director
    Dual Honeywell C-14 Remote Compass System
    Bendix-King AA-300 Radio Altimeter
    Gemelli Audio Control and Intercommunication System
    Honeywell KTR-909 UHF Communications System
    Free Flight Systems TNL2101 App+ Global Positioning System
    L3 Communications SKY497 Traffic Advisory System
    Appareo Vision 1000 Cockpit Camera System
    Artex ELT 110 Emergency Locator Beacon
    Dual Bendix-King KX-165 VHF 8.33 Communication and Navigation Systems
    Bendix-King KMR-674 Marker Receiver
    Bendix-King KDM-706 DME
    Bendix-King KR-87 Automatic Direction Finder
    Bendix-King RDR-2000 Weather Radar
    Bendix-King KT-71 Transponder
    Honeywell KMD-550 Multi Function Display
    Dual Anti Collision Beacons
    Instrument White Lighting System
  • Interior & Entertainment
    6 Place VIP Interior
    Barley leather seats
    Crew seats in cream sheepskin
    Headlining and sidewalls in cream ultra leather
    Oatmeal seat restraints
    Monuments in gold
  • EXTERIOR
    Metallic Silver with Metallic Blue Stripes
  • Additional Equipment & Information
    Rotor brake
    Dual controls
    450W rotating landing light
    Airframe hourmeter
    Air conditioning Garret ECU
    Windshield wipers (pilot/co-pilot)
    Wiper switch on cyclic grip
    Vibration absorber
    Left and right auxiliary fuel tanks

    Aluminium alloy and bonded panel fuselage
    Semi-monocoque aluminium alloy tail boom
    Two hinged jettisonable crew doors (LH and RH)
    Sliding passenger doors
    Acrylic windshield and side windows
    Acrylic overhead windows
    Quick removable tail rotor drive shaft cover
    Three-wheel retractable landing gear
    Separate baggage compartment with 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
    Grounding points

    ROTORS & CONTROLS
    Fully articulated corrosion-protect 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

    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 autostart
    Engine-mounted Fuel Management Unit (FMU) fuel pump and filter assembly
    Engine-mounted oil pump and filter assembly
    Engine oil chip detectors (two)
    Airframe mounted easy access fuel filter
    Two independent fuel systems with cross-feeding valve and control panel
    Three cell crash resistant fuel system (152 USG)
    Submerged fuel boost pump (one per system)
    Locking fuel cap
    Transmission oil chip detectors (two)
    Two transmission mounted hydraulic pumps (two) with separate reservoir

    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)
    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

    WiFi

    No

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