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Sparfell & Partners is pleased to present exclusively this beautiful 7 passenger VVIP Agusta Westland 139 helicopter, being Isle of Man registered. This AW 139 built in 2012 is equipped with a FIPS Deicing System and is ready to go. With no damage history and engines under program, it is a unique opportunity.
It is certified for EASA operations.

Agusta AW139 at a glance:
AgustaWestland an Anglo-Italian multinational helicopter design and manufacturing company, and a wholly owned subsidiary of Finmeccanica. It was formed in July 2000 when Finmeccanica and GKN merged their respective helicopter subsidiaries (Agusta and Westland Helicopters) to form AgustaWestland.
The AgustaWestland AW139 is a(n up to)15-seat medium sized twin engine helicopter developed and produced principally by AgustaWestland. It is marketed at several different roles, including VIP/corporate transport, offshore transport, fire fighting, law enforcement, search and rescue, emergency medical service,
disaster relief, and maritime patrol. The AW139 was originally designed and developed jointly by Agusta and Bell Helicopters and marketed as the Agusta-Bell AB139, it was redesignated the AW139 when Bell withdrew from the project. Since entering service in 2003, the AW139 has become one of AgustaWestland's most influential products.

The AW139 serves as the basis for AgustaWestland's wider business strategy, under which it aims to produce a standardised family of helicopters with common design features. The sharing of components and design philosophies is intended to simplify maintenance and training for operators, commonality also lowers the production costs. In 2015 AgustaWestland unveiled an AW139 variant with an increased gross weight of 7 tonnes, this enables a range of 305 km while carrying 12 passengers; existing AW139s can also be rebuilt to the newer heavy-weight model. The heavier airframe comes at the expense of decreased hot and high performance however.

The AW139 is a conventional twin-engine multi-role helicopter. It has a five-bladed fully articulated main rotor with a titanium hub and composite blades and a four-bladed articulated tail rotor. It is fitted with a retractable tricycle landing gear, the two aft wheels retract into external sponsons, which are also used to house emergency equipment. The AW139 is powered by two FADEC-controlled Pratt & Whitney Canada PT6C turboshaft engines; the FADEC system seamlessly adjusts the engines for pilot convenience and passenger comfort, and can automatically handle a single-engine failure without noticeable deviation.
The AW139 features a modular glass cockpit, a commonly installed feature is the four-axis autopilot, which enables functions such as an auto-hover capability. In July 2014, AgustaWestland announced that the global fleet had accumulated in excess of one million flight hours; by this milestone, a total of 770 AW139s had been produced.

• DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators
• DC external power receptacle
• Two nickel-cadmium batteries one 44 Ah main battery plus one 13 Ah auxiliary battery DC starter generator control units (2)
• Navigation lights (3) Anti-collision light
• External emergency landing lights on the sponsons (2)
• Fixed landing/taxing lights on the sponsons (2) Retractable/ rotating landing light
• Baggage compartment lights (3) and smoke sensor
- Engine manufacturer: Pratt & Whitney Canada
- Engine type: PT6-67C with FADEC
- Engine rating (Shp): 1’872
- Enrolled on ESP program

Engine #1 275 TT 587 Cyc
Engine #2 275 TT 587 Cyc

• Two Pratt & Whitney Canada PT6C-67C turboshaft engine
• Two independent FADEC systems with autostart and engine control functions for normal, emergency and training operations
• Two magnetic chip detectors
• Two integrated and independent engine oil coolers
• Separation firewall protection for each engine
• Fire detection system
• Fire extinguisher system (2 bottles)
• Steel engine exhausts and ejectors
• Two independent crashworthy fuel cells
• Two supply pumps on engines
• Two submerged booster pumps in fuel tank
• Two fuel filter assemblies
• Two engine back-up controls, mechanical and electrical
• Two manual engine start and ignition systems

• Main transmission with two direct drive engine inputs
• Three main transmission chip detectors/debris collectors with burning capability
• Two freewheel units
• Four strut rods for upper deck attachment and one anti-torque plate Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
• Tail gearbox with sight gauge and magnetic drain plug/chip detector
• Dual independent, redundant hydraulic systems
• Two hydraulic Power Control Modules (PCM)
• Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation
• One electrical pump for control checks on ground (engines off)
• Air conditioning compressor quill
• TCAS I KTA-970 Honeywell Bendix/King
• Weather Radar Primus 660 Honeywell removable
• Auxiliary trasversal fuel tanks 132 USG removable
• Approach plates chart holders with lights for pilot and co-pilot
• Slump protection pads provision
• MTOW extension up to 6 800 kg
• Full icing protection system/combined accessory gear box
• Moving Map Euronav V
• 5th cockpit display for Euronav V EGPWS Enhanced Vision System
• Wire Strike Protection System
• Auxiliary Heavy duty battery 27 Ah
• 10’ monitor on the separation wall
• CD, DVD, MP3 player + USB connection to an hard disk into the cabby area
• SATCOM installed in the document box on the backward bulkhead

Additional Cockpit Information
• Pilot and co-pilot crashworthy seats (with inertial reels and safety belts).
• Cockpit dome/storm light.
• Cockpit utility lights (2).
• 28 V DC cockpit/cabin power outlet. Cockpit panel sun-glare shields.
• Overhead cockpit windows sun shades.
• Floor provisions for 15-seat configuration.
• Fluorescent lighted emergency exit signs.
• Cockpit map and data case in central console.
• Two flash lights for pilot and copilot.
• Map and data cases in pilot and co-pilot doors.
• ICS panel with plug for one headset.
• Air ventilation system First aid kit.
Additional Equipment
• 1st PFD (Pilot Primary Flight Display 8’’ * 10 « colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data.
• 2nd PFD (Pilot Primary Flight Display 8‘’ * 10 « colour Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data.
• 1st MFD (Pilot Multifunction Display 8’’ * 10 colour Active Matrix Liquid Crystal Display) as partv of Honeywell Primus Epic System for visualization of flight and navigation data.
• 2nd MFD (Pilot Multifunction Display 8’’ * 10 colour Active Matrix Liquid Crystal Display) as partv of Honeywell Primus Epic System for visualization of flight and navigation data.
• One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data).
• Two Attitude and Heading Reference Systems (AHRS )
• Two Air Data Modules (ADM)
• Two flux valves
• Two Display Controllers (DC)
• Two Cursor Control Devices (CCD)
• One Reversion Control Panel (RCP)
• One Display Dimming Control Panel (DCP)
• One Stability Augmentation System (SAS) control panel
• Two Remote Instrument Controllers (RIC)
• Two Modular Avionic Units (MAU) in corporating the following major subsystems and/or functions :
• Vehicle Monitoring System (VMS) dual
• Monitor Warning System (MWS) dual
• Aural Warning Generator (AWG) single
• Central Maintenance Computer (CMC) single
• 4-axis dual Digital Automatic Flight Control System (DAFCS) Basic
• Provision for CVR/FDR data interface (single)
• Provision for CVR/FDR data interface (single)
• Flight Director System (dual) Pilot and co-pilot headsets
• Pilot and co-pilot interphone control (cyclic grip and floor switches)
• Left Modular Radio Cabinet (MRC) with the following modules :
• One VHF Comm .
• Right Modular Radio Cabinet (MRC) with the following modules:
• One VHF Comm .
• One Mode S diversity transponder
• One ADF
• One DME
• Two pedestal mounted Multi Control Function Display Units (MCDU)
• 1st radar altimeter RT-300
• 2nd radar altimeter RT -300
• Emergency Locator Transmitter (ELT)
• One flight guidance controller
• Honeywell GPS module with Flight Plan Management System (FPMS)
• Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation
• Pilot clock (digital)
• Co-pilot clock (digital)
• One magnetic compass
• One outside air temperature indicator
• Two Master Warning Lights (MWL)
• Two Master Caution Lights (MCL)
• Engine 1 fire light
• Engine 2 fire light
• Baggage compartment smoke detector light
• Dual electrical power connection for CVR/FDR (FAA requirement compliant)
• 3 armchairs leather covered (with inertial reels and safety belts)
• 4 comfortable seats leather covered (with inertial reels, safety belts and under-seat skirts)
• Armrests for comfortable seats fwd (Qty 3 per row)
• Armrests-cabinets for comfortable seats fwd (LH and RH)
• Headsets Bose ANR type (Qty 7)
• Fashion cabinet (between two armchairs) with newspaper holder
• Multipurpose cubby with 3 sliding doors
• Separation wall, closed by manual sliding glass window
• Passenger cabin sliding doors
• Super silent soundproofing
• Sliding door liners leather/leatherette covered with Passenger Service Unit
• Electrically operated pax steps (RH and LH) with boarding lights (in lieu of fixed steps)
• Nose landing gear door
• Customized VIP cabin finishing from Company selection as applicable i.a.w. prevailing airworthiness directives
• Decoration trim flat (for pax sliding doors)
• Passenger carpet (high thickness)
• Air conditioning system
• P.A. (Passenger Address) system (including loudspeakers and safety belts lights)
• ICS in cabin for all passengers
• Passenger cabin thermo acoustic double layer tinted windows
• Ripple dampers
• Active Vibration Control System (AVCS) provision
• MGB Premium grade
• Stat Com Iridium ST3100 Aircell I-pod dock station on cabinet
• AVCS removable
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