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AIRBUS EC 155BSerial Number 6586
Specifi cations
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 2
AIRCRAFT EXECUTIVE SUMMARY
Executive Summary
Aircraft Manufacturer Airbus Helicopters
Aircraft Type EC 155B
Current Registration D-HAVV
Serial Number 6586
Year of Manufacture 2001
Airframe Total Hours* 3'745
Airframe Total Cycles* 8'998
Certifi cation EASA & LBA
Home Base Germany
Cabin Confi guration 8 + 2 Seats(1)
A GREAT PEDIGREE
Sparfell & Partners is pleased to off er this 2001 AIRBUS HELICOPTERS EC 155B.
*As of September 2017
(1) 4 additional seats available for a 12 + 2 confi guration
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 3
Highlights
8 + 2 Seats Confi guration*
Maintenance Tracking Program
Satellite Phone
Painting Last Performed in 2016 at Suessmann
* 4 additional seats available for a 12 + 2 confi guration
AIRCRAFT HIGHLIGHTS
IMMACULATE CABIN
Non-smoking cabin interior with 8 + 2 seats confi guration, plus 4 additional seats available for a 12 + 2 confi guration.
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 4
AIRBUS HELICOPTERS AT A GLANCE
Because of the merger of Airbus Helicopters' former parents in 2000, the firm is now a wholly owned subsidiary of Airbus. The creation of what was then called EADS in 2000 also incorporated CASA of Spain, which itself had a history of helicopter-related activities dating back to Talleres Loring, including local assembly of the Bo105. The company was renamed Airbus Helicopters in January 2014.
It is the largest in the industry in terms turbine helicopter deliveries. More than 12,000 Airbus Helicopters are in service in around 150 countries.
Airbus Helicopters and its predecessor companies have established a wide range of helicopter firsts, including the first production turboshaft-powered helicopter in 1955; the introduction of the Fenestron shrouded tail rotor in 1968; the first helicopter certified for full flight in icing conditions in 1984; the first production helicopter with a Fly-by-wire control system in 2003; the first helicopter to use a Fly-by-light primary control system in 2003; and the first ever landing of a helicopter on Mt. Everest in 2005.
Airbus Helicopters SAS (formerly Eurocopter Group) is the helicopter manufacturing division of Airbus.
Airbus Helicopters was formed in 1992 as Eurocopter Group, through the merger of the helicopter divisions of Aérospatiale and DASA. The company's heritage traces back to Blériot and Lioré et Olivier in France and to Messerschmitt and Focke-Wulf in Germany.
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 5
SPECIFICATIONS
Airframe
Aircraft Manufacturer Airbus Helicopters
Aircraft Type EC 155B
Serial Number 6586
Year of Manufacture 2001
Year of Delivery 2001
Airframe Total Hours* 3'745
Airframe Total Cycles* 8'998
Certification EASA LBA
Maintenance Tracking Prog. Blue Eye MRX Main Rotors
#1 Blade S/N 208
#1 Blade Remaining FH*(1) 6'162(2)
#2 Blade S/N 215
#2 Blade Remaining FH*(1) 6'255(2)
#3 Blade S/N 217
#3 Blade Remaining FH*(1) 6'255(2)
#4 Blade S/N 214
#4 Blade Remaining FH*(1) 6'255(2)
#5 Blade S/N 188
#5 Blade Remaining FH*(1) 6'429(2)
Gearbox Remaining FH*(1) 1'626(3)
Tail Rotors
Blade First Lim(4) Remaining FH*(1) 2'741(2)
Blade First Lim(5) Remaining FH*(1) 2'807(2)
Blade First Lim(5) Remaining FH*(1) 4'547(2)
Gearbox Remaining FH*(1) 1'394(6)
*As of September 2017
(1) Flight Hours
(2) Interval 10'000 hours
(3) Interval 1'800 hours
(4) 8 blades
(5) 1 blade
(6) Interval 2'400 hours
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 6
SPECIFICATIONS
Inspection Last Performed Next Due
Engine #1 Overhaul - 3'500 Hours
Engine #2 Overhaul 2'885 Hours 6'385 Hours
600 Hours / 1 Year Inspection November 2017 4'345
1'200 Hours Inspection 3'147 Hours 4'467 Hours
6 Year Inspection July 2013 January 2020
8 Year Inspection June 2015 December 2023
10 Year Inspection June 2015 June 2025
12 Year Inspection April 2015 April 2027
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 7
AVIONICS
Type of Unit
ADF
ADU
AP Module
AP SFIM
CVFDR
DME
ELT Artex
FCDM
GPS
LRRA
TCAS
Transponder
VHF COMMS
VHF UHF
Weather Radar
Qty
Single
Dual
Single
Single
Single
Single
Single
Dual
Single
Single
Single
Single
Dual
Dual
Single
Unit Description
Chelton DF-431B
Thales ADU 3000
SFIM APM 2000
SFIM APHS 2310
Honeywell AR 602C
Chelton DM-411B
Artex 110-406 HM
Sextant F9111
Aerodata AD NCU 330
Thomsen ERT 160
Bendix TPU 66A
Bendix MST 67A
TRIG TY92
Chelton VN-411B (MKR)
Telephonics RT 1400
RADIO NAVIGATION AND COMMUNICATION EQUIPMENT
ADDITIONAL EQUIPMENT
Air Conditioner
Crash Resistant Fuel Tank
Surveillance Equipment Provision
Cargo Hook Provision
Sandfilter (fixed installed parts only, excl. sand filter)
Plexiglass Windshields
Hoist Provision
A I R B U S E C 1 5 5 B • D - H AV V • S & P S P E C I F I CAT I O N S • PAG E 8
CABINSUMMARY
8 + 2 Seats Confi guration*
Interior Completion in 2001
Non-Smoking Cabin
Skytrack Satellite Phone
* 4 additional seats available, for a 12 + 2 confi guration
#1 CABIN CONFIGURATION
#2 CABIN CONFIGURATION
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.