| Number |
2025-0128 |
| Issued by |
 Europe |
| Issue date |
2025-06-03 |
| Effective date |
2025-06-10 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT XWB
-
Trent XWB-75
-
Trent XWB-79
-
Trent XWB-79B
-
Trent XWB-84
-
Trent XWB-97
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0182R1 dated 09 October 2024.
|
| Publication(s) and related information |
Rolls-Royce NMSB Trent XWB 72-AL167 original issue dated 18 September 2024, or Revision 1 dated 03 October 2024, or Revision 2 dated 06 May 2025.
Rolls-Royce NMSB Trent XWB 72-AL165 original issue dated 05 September 2024, or Revision 1 dated 06 September 2024, or Revision 2 dated 11 September 2024, or Revision 3 dated 18 September 2024, or Revision 4 dated 22 November 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
25-072 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 08 May 2025 as PAD 25-072 for consultation until 22 May 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.
|
