| Number |
2011-0080R1 |
| Issued by |
 Europe |
| Issue date |
2012-11-15 |
| Effective date |
2012-11-27 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
|
| Revision |
This AD revises EASA AD 2011-0080 dated 06 May 2011.
|
| Correction |
This AD has been republished to correct typographical errors in the Reason.
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce NMSB RB211-72-AG456 dated 09 September 2010.
Rolls-Royce SB 72-AG705 dated 13 July 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
11-038 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 05 April 2011 as PAD 11-038 for consultation until 03 May 2011. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[dot]easa.europa[dot]eu.
4. For any question concerning the technical content of the requirements in this AD, please contact your designated Rolls-Royce representative or download the publication from your Aeromanager account at www.aeromanager.com.
|
