Agusta Westland AW109S GRAND G-LUGS · - VSI - LCD EADI and EHSI ... interchangeable composite...
Transcript of Agusta Westland AW109S GRAND G-LUGS · - VSI - LCD EADI and EHSI ... interchangeable composite...
AV I AT I O N
V O L A R E
AW109S GRAND
G-LUGSAgusta Westland
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VIP 2009 AW109S - one previous owner – always hangaredExcellent maintenance records - maintained by a Leonardo Authorised Service CentreHighest specification five seat VIP interior including rear cabinet barOptional equipment including weather radar - TAS 497 set of three drawers - baggage compartment extension (2.3m)
AW109S GRAND
G-LUGS
Aircraft:
Puchase Options:
AW A109S GRAND
Serial No.
Registration:
Year of Manufacture:
Asking Price: Cost on application
2215
G-LUGS
2009
Certification:
Airframe: Total time
EASA & FAA
2,700 hrs
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Two forward facing seats with rear cabinet bar
VIP INTERIOR Five Seats
Fold out tables and champagne cabinet in carbon fibre
Three aft facing seats with foldable armrest
Light brown floor carpeting with carbon fibre kick plates
Four-point shoulder harness with inertia reels and safety belts on all seats
Three under seat carbon fibre storage drawers
Two beige sheepskin breathable crew seats
Dual USB Chargers
Dual iPad mini EFB with mounts
7 BOSE noise cancelling headsets
EXTERIOR FINISHING
Finished in customised factory paint - metallic black with a metallic silver and blue stripe
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Weather radar
ADDITIONAL OPTIONAL EQUIPMENT Five Seats
Skywatch TAS 497
Emergency float provisions
Set of three drawers
Fuel cap with key
SINGLE PILOT IFR (EASA/FAA) AVIONIC PACKAGE (KING-GARMIN)
Electric folding step
AC system (two inverters)
LCD EADI and EHSI
Vertical gyros (no. 1), Flightline system 46060-11
Vertical gyros (no. 2), Jet Electronics VG 208
Autopilot Honeywell 3 Axis Duplex SP-711
ADF King KR87
Transponder King KT-73 (Mode S)
Garmin GNS 530 Nav-Com-GPS 8.33
Garmin GNS 430 Nav-Com-GPS 8.33
DME King KDM-706A
King KMR-675 Marker Beacon
ICS pilot including:
Pilot/co-pilot control panel, NAT AA95-896TSOMode S controller AA 31-002Audio cabin control system AA 82-060
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Co-pilot flight/navigation instruments including the following instruments:
AVIONIC EQUIPMENT Factory Installed
Honeywell Radio Altimeter RT-300
Artex C406-2HM ELT
Honeywell KMD 550 moving map
EFIS pilot/co-pilot on command switch
AIRFRAME
- Barometric altimeter- Air Speed Indicator- VSI- LCD EADI and EHSI
Four-point shoulder harness with inertia reels and safety belts on all seats
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
Aluminium alloy and bonded panel fuselage
Semi-monocoque aluminium alloy tail boom
Two hinged jettisonable crew doors (LH and RH)
Two passenger sliding doors with jettisonable windows (LH and RH) with 1.40m opening
Acrylic windshield and side windows
Acrylic overhead windows
Quick removable tail rotor drive shaft cover
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
ENCLOSURE 1 AW109S BASELINE AIRCRAFT
AW109S GRAND
G-LUGSAgusta Westland
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POWER PLANT, FUEL SYSTEM & ELECTRIC DRIVE SYSTEM
Three cell crash resistant fuel system (152 USG)
Engine-mounted Fuel Management Unit (FMU) fuel pump and filter assembly
Two independent electronic control systems (FADEC) with normal emergency and training operation modes and autostart
Engine-mounted oil pump and filter assembly
Airframe mounted easy access fuel filter
Two Pratt & Whitney PW207C turboshaft engines
Two independent fuel systems with cross-feeding valve and control panel
Engine oil chip detectors (two)
Submerged fuel boost pump (one per system)
Locking fuel cap
Two Pratt & Whitney PW207C turboshaft engines
Two transmission mounted hydraulic pumps (two) with separate reservoir
960 shp for takeoff and 900 shp coninuous operation main transmission / with two direct drive inputs
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
ROTORS & CONTROLS
Cyclic and collective controls powered by two separate hydraulic systems
Two composite tail rotor blades semi-rigid delta hinged type individually changeable
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
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External power receptacle
Battery relay / external power relay
External power relay
24 V DC 27 Ah nickel cadmium battery withtemperature probe
Distribution buses (one battery, two essential, two emergency, two main)
Two interconnecting bus relays
Two 160 A self-cooled starter generators
Two voltage regulators
Radio master switch
Two 250 W landing lights
Two anti-collision lights
Two DC ammeters (on IDS display)
Instrument lights with dimming switch
Two utility lights
Two DC voltmeters (on IDS display)
Two 150 W taxing lights
ELECTRICAL SYSTEM ADDITIONAL EQUIPMENT
Windshield wipers (pilot/co-pilot)
Engine chip burner
Engine compartment fire extinguisher
Rotor brake
Airframe hourmeter
Engine compartment fire extinguisher
Dual controls
450W rotating landing light
Vibration absorber
Wiper switch on cyclic grip
Air conditioning Garret ECU
Left and right auxiliary fuel tanks
MISCELLANEOUS
Flight manual and technical publications
Air intake/exhaust covers
Ground tools kit including lifting tool, tow bar and wheel chocks
Pitot tube covers
Tie-down fittings provisions
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+44 (0)800 888 6599 [email protected] www.volareaviation.co.uk
This aircraft is for sale subject to prior sale and as of January 2018
AV I AT I O N
V O L A R E
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