| Number |
2011-0066 |
| Issued by |
 Europe |
| Issue date |
2011-04-11 |
| Effective date |
2011-04-25 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2010-0161, dated 03 August 2010.
|
| Publication(s) and related information |
Turboméca Mandatory Service Bulletin (MSB) A333 73 0809 version B,
dated 18 January 2011: Ref [1].
Turboméca Mandatory Service Bulletin (MSB) A333 73 0811 version B,
dated 18 January 2011: Ref [2].
TM 333 2B2 Maintenance Manual X 333 H8 450 2 Update 17
Airworthiness Limitation Section Task 05-10-00-150-801-A01 Authorized
In-Service Life Limits, Counting/Recording of cycles and Table of
Mandatory Maintenance Tasks: Ref [3].
TM 333 2B2/2M2 Overhaul Manual X 333 H8 500 2 Update 15
Airworthiness Limitation Section Task 05-10-00-150-801-A01 Authorized
In-Service Life Limits, Counting/Recording of cycles and Table of
Mandatory Maintenance Tasks: Ref [4].
TM 333 2M2 Maintenance Manual X 333 B2 450 2 Update 8 Airworthiness
Limitation Section Task 05-10-00-150-801-A01 Authorized In-Service Life
Limits, Counting/Recording of cycles and Table of Mandatory
Maintenance Tasks: Ref [5].
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The required actions and the risk allowance have granted the
issuance of a Final AD with Request for Comments, postponing the
public consultation process after publication.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
