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ADs [at] easa.europa [dot] eu
|
| Number |
26-062 |
| Issued by |
 Europe |
| Issue date |
2026-05-08 |
| EASA approval number |
|
| ATA Chapter |
05 |
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 2025-0119 dated 26 May 2025.
|
| Publication(s) and related information |
Rolls-Royce Trent XWB TLM PCM-TRENTXWB-K0680-TIME0-01, Revision 064 dated
01 February 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 05 June 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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