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AIRCRAFT EXECUTIVE SUMMARY
Executive Summary
Aircraft Manufacturer AgustaWestland
Aircraft Type AW139
Current Registration UP-AW902
Serial Number 31116
Year of Manufacture 2008
Airframe Total Hours* 4,900
Airframe Total Cycles* 13'570
Certifi cation EASA
Home Base Atyrau, Kazakhstan
Cabin Confi guration 11 + 2 Seats
A GREAT PEDIGREE
Sparfell & Partners is pleased to off er, for immediate sale, this 2008 AGUSTAWESTLAND AW139.
*As of September 2017
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Highlights
One Owner Since New
11 + 2 Seats Confi guration(1)
Maintenance Tracking Program
EASA Certifi cation
4-Axis Dual Digital Automatic Flight Control System
Pop-Out Floats
Freon Air Conditioning
Auxiliary Fuel Tank
Health & Usage Monitoring System
(1) Can be converted to 15 + 2 Seats Confi guration
AIRCRAFT HIGHLIGHTS
IMMACULATE CABIN
High-density seating with 11 + 2 cabin interior. This helicopter can be converted to 15 + 2 cabin confi guration.
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AGUSTAWESTLAND AT A GLANCE
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 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 AgustaWestland AW139 is a(n up to)15-seat medium sized twin-engined 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.
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SPECIFICATIONS
Airframe
Aircraft Manufacturer Agusta
Aircraft Type AW139
Serial Number 31116
Year of Manufacture 2008
Year of Delivery 2008
Airframe Total Hours* 4'900
Airframe Total Cycles* 13'570
Certification EASA
Maintenance Tracking Prog. AMOS
Engines
Manufacturer Pratt & Whitney
Type PWC PT6C- 67C
#1 Engine Total Hours* 4'900(1)
#1 Engine Total Cycles* 4'889
#2 Engine Total Hours* 4'900(2)
#2 Engine Total Cycles* 4'889
*As of September 2017
(1) Just overhauled
(2) Due at 5'200 hours
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SPECIFICATIONS
Major Inspection Status
Engine #1 recently overhauled in Italy
Engine #2 has 200 hours remaining before overhaul
Inspection Last Performed Next Due
Last Engine #1 Overhaul 4'900 Hours (April 2017) 10'000 Hours
Last Engine #2 Overhaul - 5'200 Hours
1 Year Inspection October 2016 October 2017
4 Years Inspection November 2016 November 2020
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SPECIFICATIONS
Performance
Maximum Speed 160 Kts
Long Range Speed 140 Kts
Seats Full Range 460 Nm
Maximum Ceiling 20'000 ft
Service OEI (One Engine Inoperative) 11'600 ft
Hover IGE 15'360 ft
Hover OGE 8'130 ft
Engines (x2) PT6C-67C
Thrust Level in Shaft Horsepower (each) 1'531 shp
Consumption 110 Gal./hr*
Passenger Configuration 15
Cabin Volume 282 Cu. ft
Baggage Volume 120 Cu.ft
Source: Conklin & de Decker
* Source: Seller
Weights
LBS KG
Maximum Take-Off (MTOW) 14'991 6'800
Maximum Landing (MLW) 14'991 6'800
Equipped Empty (EEW) 10'229 4'640
Maximum Usable Fuel 4'405 1'998
Source: Seller
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AVIONICS
Type of Unit
ADF
Autopilot
Compass
DME/VOR/ILS
FMS
FPMS
Hi Frequency
Radar Altimeter
TCAS
Weather Radar
ADF
Communication Radios
VHF/FM
ICS
Passenger Public Address System
Crew Headset
Automatically activated
EFIS
Flight Director
Flight Tracking System
GPS
Navigation Radios
TAWS
Transponder
Underwater Locator Transmitter
Qty
Single
Dual
Dual
Single
Single
Single
Single
Dual
Single
Single
Single
Dual
Single
Single
Single
Single
Single
Single
Dual
Single
Single
Dual
Single
Single
Single
Unit Description
Honeywell
Honeywell Primus AFCS 4-axis
AHRS
Honeywell
Honeywell FMS w/GPS
GPS module with Flight Plan Management System
Unit
Honeywell RT-300
TCAS-I provisions
Honeywell Primus 660
Unit
Honeywell Primus
Marine Radio
Pilot Intercom System
Clearly audible at all passenger seat locations
David Clark Aviation Headset H10-13.4 or similar
ADELT
Honeywell Primus 3-tube 8x10-inch
Honeywell Primus AFCS
DSAT 300E
Bendix/king Skyforce Skymap IIIC
Honeywell Primus
EGPWS
Honeywell Mode S
Beacon - Integral with CVR
RADIO NAVIGATION AND COMMUNICATION EQUIPMENT
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AVIONICS
Type of Unit
Flight Data Recorder
Cockpit Voice Recorder
HDFM
Qty
Single
Single
Single
Unit Description
FDR provisions
CVR provisions
With QA data download
RECORDING/MONITORING EQUIPMENT
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CABINSUMMARY
11 + 2 Seats Configuration*
Non-Smoking Cabin
Length 8’85” ft/in
Height 4’70” ft/in
Width 7’20” ft/in
Cabin Volume 282 Cu. ft
Baggage volume 120 Cu. ft
Number of Baggage 21
Source: Conklin & de Decker
* Can be converted to 15 + 2 Seats Configuration
Safety / Offshore Modifications
12-15 Padded crash worthy comfortable seats fabric or leatherette covered disposed on 3 rows*
Separate 4 points seatbelts
Health & Usage Monitoring System (HUMS)
ADELT (2-frequency Automatic Deployable ELT w/ GPS interface) in lieu of standard ELT
Emergency floats
Life rafts (Qty 2) up to 17 passengers each
Helicopter Emergency Exit Lighting System (HEELS)
TRON SART beacon
*With inertial reels and safety belts
Terminal C318 chemin des papillons1215 Geneva AirportSwitzerland
Phone +41 22 787 08 77 | [email protected]
WWW.SPARFELL-PARTNERS.COM
Disclaimer: These specifi cations are presented as introductory information only. They do not consti-tute representations or warranties of any kind. Accordingly, you should rely on your own inspection of this aircraft. The aircraft is subject to sale, and / or removal from the market without prior notice.