Number |
2015-0105R1 |
Issued by |
Europe |
Issue date |
2015-08-18 |
Effective date |
2015-08-18 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
72 |
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This AD revises EASA AD 2015-0105 dated 10 June 2015, which superseded EASA AD 2014-0168 dated 16 July 2014.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2014-0168 dated 16 July 2014.
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-H673 dated 30 January 2014, or Revision 1 dated 21 February 2014, or NMSB RB.211-72-AH673 Revision 2 dated 27 June 2014.
Rolls-Royce NMSB RB.211-72-AJ035 dated 11 May 2015, or Revision 1 dated 20 May 2015, or Revision 2 dated 10 August 2015.
Rolls-Royce SB RB.211-72-H754 dated 01 October 2014, or Revision 1 dated 29 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
15-056 |
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 May 2015 as PAD 15-056 for consultation until 02 June 2015. 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.
|