Number |
2018-0202R1 |
Issued by |
Europe |
Issue date |
2018-09-25 |
Effective date |
2018-09-25 |
EASA approval number |
|
Contributor |
EASA Propulsion Section |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-535
-
RB211-535E4-37
-
RB211-535E4-B-37
-
RB211-535E4-C-37
|
Revision |
This AD revises EASA AD 2018-0202 dated 11 September 2018.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded United Kingdom (UK) CAA AD 002-01-2000 dated January 2000.
|
Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-C879 original issue dated 11 January 2000, or Revision 1 dated 30 June 2000, or Revision 2 dated 4 January 2002, or Revision 3 dated 9 October 2002, or Revision 4 dated 2 April 2004, or Revision 5 dated 8 March 2007, or Revision 6 dated 14 December 2007, or Revision 7 dated 1 May 2009, or Revision 8 dated 18 November 2015, or Alert NMSB RB.211-72-AC879 Revision 9, dated 23 April 2018.
Rolls-Royce SB RB.211-72-C946 original issue dated 29 September 2000, or Revision 1 dated 28 August 2001, or Revision 2 dated 26 September 2002, or Revision 3 dated 22 September 2008, or Revision 4 dated 22 June 2010.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
18-066 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 04 May 2018 as PAD 18-066 for consultation until 01 June 2018. The
Comment Response Document can be found in the EASA Safety Publications Tool, in the
compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.
|