| Number |
2016-0223 |
| Issued by |
 Europe |
| Issue date |
2016-11-08 |
| Effective date |
2016-11-22 |
| 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2010-0087 dated 05 May 2010, including its Correction dated 06 May 2010.
|
| Publication(s) and related information |
Rolls-Royce ALS of the RR Trent 800 Engine TLM, task 05-10-01-800-801, or task 05-10-01-800-802, both dated 15 June 2016.
Rolls-Royce SB RB.211-72-C768 original issue dated 8 October 1999, or Revision 1 dated 25 October 2000, or Revision 2 dated 25 September 2006, or Revision 3 dated 3 January 2007, or Revision 4 dated 16 April 2010.
Rolls-Royce SB RB.211-72-F867 original issue dated 1 February 2008, or Revision 1 dated 16 April 2010.
Rolls-Royce NMSB RB.211-72-G150 original issue dated 23 April 2009.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-129 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 08 September 2016 as PAD 16-129 for consultation until 06 October 2016. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
