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ADs [at] easa.europa [dot] eu
|
| Number |
26-137 |
| Issued by |
 Europe |
| Issue date |
2026-11-12 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-A
-
Trent 1000-A2
-
Trent 1000-AE
-
Trent 1000-AE2
-
Trent 1000-C
-
Trent 1000-C2
-
Trent 1000-CE
-
Trent 1000-CE2
-
Trent 1000-D
-
Trent 1000-D2
-
Trent 1000-E
-
Trent 1000-E2
-
Trent 1000-G
-
Trent 1000-G2
-
Trent 1000-H
-
Trent 1000-H2
-
Trent 1000-J2
-
Trent 1000-K2
-
Trent 1000-L2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0143 dated 08 July 2025.
|
| Publication(s) and related information |
Rolls-Royce NMSB TRENT 1000 72-AK965 original issue dated 19 May 2023, or Revision 1 dated 01
August 2023, or Revision 2 dated 08 November 2023, or Revision 3 dated 09 May 2025.Revision 4 dated 02 November 2026.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 26 November 2026. 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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