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Might want to touch base with DOM's of organizations operating EC 120B's with Arrius 2F engines. This was new this morning..........click on search, click on list all recent ADs

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TUBOMECA turboshaft engines Arrius 2F which equip EC 120B helicopters. FR UF-2005-073 EMERGENCY AIRWORTHINESS DIRECTIVE - IMMEDIATE GROUNDING

 

 

TURBOMECA TUBOMECA turboshaft engines Arrius 2F which equip EC 120B helicopters. FR UF-2005-073 EMERGENCY AIRWORTHINESS DIRECTIVE - IMMEDIATE GROUNDING

 

Go to.......http://www.tc.gc.ca/aviation/applications/cawis-swimn/awd-lv-cs1401.asp?rand=

 

HBD

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EMERGENCY AIRWORTHINESS DIRECTIVE (EAD) PUBLISHED BY DIRECTION GENERALE DE L’AVIATION

 

CIVILE (FRANCE) ON BEHALF OF EASA.

 

THIS TEXT IS NOT SENT TO FOREIGN OPERATORS OF AIRCRAFT NOT REGISTERED IN FRANCE.

 

IT IS UP TO THE NATIONAL AUTHORITIES TO FORWARD IT TO THEM ON RECEIPT.

 

 

 

N° UF-2005-073 – TURBOMECA – ARRIUS 2F

 

 

 

SUBJECT: Immediate Grounding

 

 

 

1. EFFECTIVITY:

 

 

 

This Airworthiness Directive (AD) applies to TURBOMECA turboshaft engines Arrius 2F which equip EC 120B

 

helicopters.

 

 

 

2. REASON:

 

 

 

Following an accident involving an EC120B, the initial investigation of the Arrius 2F engine showed that one HP

 

blade was totally released from the HP disk. This blade was contained inside the containment ring.

 

 

 

The preliminary examination of the engine parts showed that the standard of one ferrule initiated a disturbance in

 

the secondary air system used to cool the HP turbine.

 

 

 

3. MANDATORY ACTIONS AND COMPLIANCE TIMES:

 

 

 

3.1. Following actions are made mandatory from the effective date of this AD.

 

For all Arrius 2F modules 2 listed in Alert Fax TURBOMECA n°057/05/DSO/TM: immediate grounding.

 

 

 

3.2. Flights may be resumed after the engine having been treated in a repair center.

 

 

 

4. REFERENCE PUBLICATION:

 

 

 

Alert Fax TURBOMECA n° 057/05/DSO/TM, April 26, 2005.

 

 

 

5. EFFECTIVE DATE:

 

 

 

Upon receipt of the EAD issued on April 27, 2005.

 

 

 

6. REMARKS:

 

 

 

For any questions concerning the technical content of the requirements in this EAD, please contact :

 

 

 

Arrius Service engineering manager

 

Customer Support

 

TURBOMECA

 

Fax: +33 5 59 74 4515

 

 

 

7. APPROVAL:

 

 

 

This EAD is approved under EASA reference No 2005-3835 dated April 27, 2005.

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16 currently registered in Canada. It seems that this AD only affects certain engines. MAG, any idea how many engines are out there worldwide that require attention?

 

 

Mark Common Name Model Owner name Owner Registered Since Serial Number

1 C-FCOS Eurocopter EC120B Fox Aviation Inc 1999-03-18 1022

2 C-FDNR Eurocopter EC120B Province Of Nova Scotia, Depar 2005-04-15 1382

3 C-FEPS Eurocopter EC120B City Of Edmonton 2001-07-31 1035

4 C-FGBA Eurocopter EC120B Heli-Inter Inc. 1999-10-07 1033

5 C-FJDZ Eurocopter EC120B Memento Mori Investments Limit 2002-11-05 1002

6 C-FLCN Eurocopter EC120B Eurocopter Canada Limited 2005-01-24 1055

7 C-GEXM Eurocopter EC120B Heli/Express Inc. 1999-06-16 1028

8 C-GHBB Eurocopter EC120B 602472 B.C. Ltd 2001-07-18 1091

9 C-GHNI Eurocopter EC120B Industries Cover Inc./Cover In 2003-09-25 1131

10 C-GIJZ Eurocopter EC120B Phoenix Heli-Flight Inc. 2001-08-16 1050

11 C-GJUH Eurocopter EC120B Silverline Helicopters Inc. 2005-02-22 1267

12 C-GLCN Eurocopter EC120B CFLCN Inc. 2004-11-23 1325

13 C-GRTA Eurocopter EC120B 171817 Canada Inc 2000-10-20 1076

14 C-GRTN Eurocopter EC120B Great Slave Helicopters Ltd 2002-07-26 1058

15 C-GYDC Eurocopter EC120B 3939421 CANADA INC 2003-12-03

16 C-GYRP Eurocopter EC120B York Regional Police 2003-01-27

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3bx2

 

After the release of the TC AD I contacted the FAA regarding the AD, I was told that they were a little slower in releasing the document but as of this afternoon I received the e-mail prior to it going on their site so here it is......

 

http://www.airweb.faa.gov/Regulatory_and_G...BD?OpenDocument

 

****, no worse that the 250-C18 "Blue Ribbon" engines prior to the installation of the two and a half bearing or the Jet Ranger "widow makers" tossing blades..........ah, those were the days. That will teach Bell to use a cheaper vendor for making wire for the TT straps, used 7 miles of wire and not 9. Now if only they kept the old orange garlock seals for the freewheel instead of speedi sleeves and the 406 seals for the forward cap assembly.

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