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ADs [at] easa.europa [dot] eu
|
| Number |
26-114 |
| Issued by |
 Europe |
| Issue date |
2026-09-24 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-AE3
-
Trent 1000-CE3
-
Trent 1000-D3
-
Trent 1000-G3
-
Trent 1000-H3
-
Trent 1000-J3
-
Trent 1000-K3
-
Trent 1000-L3
-
Trent 1000-M3
-
Trent 1000-N3
-
Trent 1000-P3
-
Trent 1000-Q3
-
Trent 1000-R3
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0206R1 dated 18 December 2025.
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AK316 original issue dated 09 April 2019, or Revision 1 dated 18 April 2019, or Revision 2 dated 30 April 2019, or Revision 3 dated 16 July 2019, or Revision 4 dated 10 May 2024, or Revision 5 dated 30 May 2025, or Revision 6 dated 29 July 2025, or Revision 7 dated 09 September 2026.
Rolls-Royce SB TRENT 1000 72-J550 original issue dated 21 November 2017, or Revision 1 dated 22 March 2022.
Rolls-Royce SB TRENT 1000 72-L042 original issue dated 24 January 2024.
Rolls-Royce SB TRENT 1000 72-K335 original issue dated 06 March 2025.
Rolls-Royce SB TRENT 1000 72-L088 original issue dated 17 February 2026.
Boeing Aircraft Maintenance Manual (AMM) Task B787-A-R72-00-00-23C-280C-A.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
|
| Remarks |
1. This Proposed AD will be closed for consultation on 22 October 2026.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@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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