| Number |
2016-0120 |
| Issued by |
 Europe |
| Issue date |
2016-06-17 |
| Effective date |
2016-07-01 |
| EASA approval number |
|
| 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2014-0243R1 dated 10 December 2014, including the
Correction dated 23 March 2015.
|
| 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.
Rolls-Royce SB RB.211-73-AJ366 dated 03 May 2016.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-064 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 May 2016 as PAD 16-064 for consultation until 07 June 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.
|
