Agusta AW 139 - 2012 - FIVESTARS Cabin Interior (7 seats) € 8.800.000

Agusta AW 139 - 2012 - FIVESTARS Cabin Interior (7 seats)
Agusta AW 139 - 2012 - FIVESTARS Cabin Interior (7 seats)
Agusta AW 139 - 2012 - FIVESTARS Cabin Interior (7 seats)
Agusta AW 139 - 2012 - FIVESTARS Cabin Interior (7 seats)

Listed Price

€ 8.800.000
approx. $ 9,728,314.70
approx. € 8.800.000
approx. 35,734,833.56 د.إ
approx. $ 14,403,071.49
approx. $ 12,954,535.16
approx. CHF 9,607,586.31
approx. ¥ 68,894,951.89
approx. £ 7,961,720.85
approx. $ 76,291,019.88
approx. 65.060.128,06 kn
approx. $ 192,668,309.57
approx. 87.468.153,04 kr
approx. 638.992.190,82 ₽
approx. 94 309 483,34 kr
approx. ฿ 298,951,052.43
approx. R 147,685,341.20
approx. $ 305,011,053.13
approx. ₱ 509,510,754.21
approx. 226 698 927,23 Kč
approx. ₨ 350,703,274.02
approx. $ 13,497,180.56
approx. $ 8,094,813.93
approx. $ 6.956.474.636
approx. B/. 9,728,314.70
approx. $ 19,456,629.40
approx. ₹ 697,756,805.40
approx. ¥ 1,037,417,752
approx. $ 26,291,256.90
approx. $ 15,264,893.17
approx. £ 7,961,720.85
approx. R$ 39.588.403,85
approx. ₪ 34,183,741.33
approx. ر.ع. 3,745,654.097
approx. 38 316 553,17 zł
approx. 21,273,499.19 $
approx. $ 33.002.216.693,79
approx. 1,050,119,623 Fr
approx. $ 9,728,314.70
approx. 35,372,638.67 ر.ق
approx. ₡ 5.491.309.141,96
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Details

  • VAT Type: VAT Excluded
  • Year: 2012
  • Location: Saint Petersburg, Russian Federation
  • Helicopter type: Twin Engine
  • TTAF: 272
  • Max range: 1000 km (621 mi)
  • Max take off weight: 6400 kg (14110 lbs)
  • Capacity: 7
  • Serial number: 31392
  • Condition: Used

Description

Ladies and Gentlemen,   

we are very pleased to announce that now, along with our vehicles, you also have an unparalleled opportunity to purchase helicopters and airplanes from Hollmann International - of course, as always relying on our top service and creditableness known for many years.   

Today, we have a great pleasure to present to your attention ultra reliable helicopter:

Agusta AW 139 - 31392


  • The Agusta AW 139 helicopter, serial number 31392, was manufactured in Italy in April 2012 at Agusta Westland’s main company, Finmeccanica.
  • Since the beginning of operation, the helicopter flew 248: 57 hours.
  • The helicopter is equipped with two gas turbine engines RT6S-67C with an electronic control system. Engines have 218: 56 flight hours.

  - We are firmly convinced that our offer is the most attractive in the market since we are dealing with the ultimate owner directly -   

We would like to draw your attention to the equipment and description of the machines in the application. 

BASIC AIR CRAFT

  • Aluminium alloy fuselage
  • Acrylic windshields
  • Overhead cockpit windows
  • Lower cockpit windows
  • Cockpit ram air adjustable outlets
  • Forced fan ventilation
  • Bleed air heater and defroster with air noise suppressions
  • Heated Pitot tubes (2) with Pitot heat failure warning (2)
  • Heated static intakes (2)
  • One cockpit and one passenger cabin fire extinguisher
  • Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side)
  • Plug-in sliding doors (2) for passenger cabin access with four locking latches
  • Passenger doors stop in fully open position
  • Six cabin push-out emergency exit windows (two on each passenger cabin door)
  • Baggage compartment with two lockable baggage compartment doors (LH and RH)
  • Baggage compartment cargo tie-down fittings
  • Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear)
  • Structural provisions for nose landing gear doors
  • Landing gear mooring
  • Upper deck mooring provisions
  • Hoisting and jacking fittings
  • Tail boom and vertical fin
  • Stabilizers with composite “winglets”
  • Pilot and co-pilot windshield wipers
  • Maintenance steps for access to upper deck on both sides
  • Upper deck cowlings (one front forward sliding, two side opening for engine access)
  • Steps for cockpit access
  • Anti-vibration masses (2) under cabin floor

ROTORS AND CONTROLS


  • Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers
  • Rotating M/R flight controls
  • Main rotor hub beanie
  • Main dual servo actuators (3)
  • Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers
  • Rotating T/R flight controls
  • One T/R dual servo actuator force trim system
  • Pilot fixed flight controls (cyclic, collective, anti-torque pedals)
  • Co-pilot fixed flight controls (cyclic, collective, anti-torque pedals)
  • Dual digital 3-axis linear actuators Rotor brake
  • Provision for mam rotor tracking (magnetic pick-up)

POWER PLANT AND FULL SYSTEM

  • Two Pratt & Whitney Canada PT6C-67C turboshafl engines
  • 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

TRANSMISSION DRIVE SYSTEM AND HYDRAULIC SYSTEM

  • 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

ELECTRICAL SYSTEMS

  • 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

INTERIOR

  • 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 co-pilot
  • Map and data cases in pilot and co-pilot doors
  • ICS panel with plug for one headset
  • Air ventilation system First aid kit

FIVESTARS Cabin Interior (7 seats)

  • 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 doors
  • 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

PAINTING

  • Standard colour scheme from Company paint selection, solid colour

MISCELLANEOUS / GROUNDEQUIPMENT

  • Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (1)
  • Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue
  • Tie-down assemblies for main rotor blades (5)
  • Tail rotor blades flapping block (1)
  • Main rotor blades sock pole (1)
  • Main landing gear wheel chocks (2)
  • Main rotor balance and tracking chart, tail rotor balance chart
  • Nose landing gear centre pin (1) and landing gear handle locking pin (1)
  • Jacking dome assy (1)
  • Tow bar (1)
  • Loose equipment bag (1)

We are very happy to provide you with any additional information with regard to our premium helicopters and remain at your disposal for any questions you may have.

Hollmann International GmbH & Co. KG
Charlotte Auerbach Str 4 
28816 Stuhr

Mob:       +49 175 / 70 35 774
Office:      +49 421 / 673 14 348

Elite Seller

For Sale by

Hollmann International GmbH

Charlotte-Auerbach-Str. 4
28816
Stuhr
Germany
Member since 2016
Konstantin Hollmann
Responsible agent
Konstantin Hollmann
Mr.

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