| Number |
2024-0116 |
| Issued by |
 Europe |
| Issue date |
2024-06-21 |
| Effective date |
2024-07-05 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| 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
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0217R1 dated 08 March 2024.
|
| Publication(s) and related information |
Rolls-Royce Trent XWB TLM TRENTXWB-K0680-TIME0-01, Revision 57 dated 01 May 2024, Modules "Airworthiness Limitations (Mandatory Parts Lives)" TRENTXWB-A-05-10-01-00A01-030A-D and Modules "Airworthiness Limitations (Mandatory Inspections)" TRENTXWB-A-05-20-01-00A01-030A-D.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
24-051 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 14 May 2024 as PAD 24-051 for consultation until 11 June 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.
|
