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ADs [at] easa.europa [dot] eu
|
| Number |
25-093 |
| Issued by |
 Europe |
| Issue date |
2025-06-26 |
| 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 2024-0102 dated 17 May 2024.
|
| Publication(s) and related information |
RR Alert NMSB RB.211-72-AL191 original issue dated 30 May 2025.
RR NMSB RB.211-72-G702 original issue dated 23 May 2011, or Revision 1 dated 15 January 2013.
RR NMSB RB.211-72-G872 original issue dated 03 April 2012, or Revision 1 dated 02 July 2012, or Revision 2 dated 08 March 2012, or Revision 3 dated 11 August 2015.
RR NMSB RB.211-72-H311 original issue dated 08 March 2013.
Rolls-Royce Alert 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.
RB211 Trent 700 Engine Manual (E-TRENT-1RR).
RB211 Trent 700 Time Limit Manual (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 Aircraft Maintenance Manual. |
| Remarks |
1. This Proposed AD will be closed for consultation on 03 July 2025.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.
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