Number |
2017-0006 |
Issued by |
Europe |
Issue date |
2017-01-10 |
Effective date |
2017-01-24 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
73 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-535
-
RB211-535E4-37
-
RB211-535E4-B-37
-
RB211-535E4-C-37
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2014-0123 dated 15 May 2014.
|
Publication(s) and related information |
Rolls-Royce SB RB.211-73-H131 original issue dated 10 May 2013, or Revision 1 dated 02 September 2014.
Rolls-Royce SB RB.211-73-G230 original issue dated 12 November 2009, or Revision 1 dated 07 July 2011, or Revision 2 dated 20 December 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
16-158 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 November 2016 as PAD 16-158 for consultation until 08 December 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.
|