Number |
2014-0243R1 |
Issued by |
Europe |
Issue date |
2015-03-23 |
Effective date |
2014-12-10 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
73 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
|
Revision |
This AD revises EASA AD 2014-0243 dated 06 November 2014, which superseded EASA AD 2014-0089 dated 15 April 2014.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2014-0089 dated 15 April 2014.
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-73-AH522 dated 20 September 2013, or Revision 1 dated 18 March 2014.
Rolls-Royce SB RB.211-73-F343 dated 08 November 2006, or Revision 1 dated 14 May 2009, or Revision 2 dated 1 July 2009, or Revision 3 dated 15 July 2009, or Revision 4 dated 26 May 2011.
Rolls-Royce NMSB RB.211-73-AH837 dated 09 September 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
14-140 |
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 10 September 2014 as PAD 14-140 for consultation until 08 October 2014. The Comment Response Document can be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|