| Number |
2024-0182R1 |
| Issued by |
 Europe |
| Issue date |
2024-10-09 |
| Effective date |
2024-10-16 |
| 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 |
This AD revises EASA AD 2024-0182 dated 19 September 2024, which superseded EASA AD 2024-0174-E dated 05 September 2024.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| 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.
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.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until 17 October 2024. 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.
|
