| Number |
2024-0102 |
| Issued by |
 Europe |
| Issue date |
2024-05-17 |
| Effective date |
2024-05-31 |
| EASA approval number |
|
| 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2018-0188R1 dated 05 September 2018.
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-G702 original issue dated 23 May 2011.
Rolls-Royce NMSB RB.211-72-G872 original issue dated 02 April 2012, or Revision 1 dated 02 July 2012, or Revision 2 dated 08 March 2013.
Rolls-Royce NMSB RB.211-72-H311 original issue dated 08 March 2013.
Rolls-Royce NMSB RB.211-72-AH465 dated 15 July 2013, or Revision 1 dated 10 July 2015, or
Revision 2 dated 11 May 2016, or Revision 3 dated 27 April 2017, or Revision 4 dated 03 October 2017, or Revision 5 dated 26 July 2018, or Revision 6 dated 29 November 2019, or Revision 7 dated 08 July 2020, or Revision 8 dated 16 January 2023, or Revision 9 dated 16 February 2024.
RR Trent 700 EM E-Trent-1RR.
RR Trent 700 TLM T-Trent-1RR.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
Airbus A330 AMM Task 72-31-41. |
| PAD number |
24-043 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 12 April 2024 as PAD 24-043 for consultation until 10 May 2024. 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. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be
installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate
(STC) or other modification.
|
