| Number |
2025-0143 |
| Issued by |
 Europe |
| Issue date |
2025-07-08 |
| Effective date |
2025-07-22 |
| 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 2023-0201 dated 17 November 2023.
|
| Publication(s) and related information |
Rolls-Royce TRENT 1000 Alert NMSB 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.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-081 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 03 June 2025 as PAD 25-081 for consultation until 01 July 2025. 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.
|
