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|
| Number |
24-136R1 |
| Issued by |
 Europe |
| Issue date |
2025-03-10 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 900
-
970-84
-
970B-84
-
972-84
-
972B-84
-
972E-84
-
977-84
-
977B-84
-
980-84
|
| Revision |
This PAD is republished for additional consultation adding reference to the Rolls-Royce RB211
Trent 900 TLM T-TRENT-9RR at Revision 68 and including credit for inspections accomplished in
accordance with the Rolls-Royce TV 257089.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0039 dated 08 February 2024.
|
| Publication(s) and related information |
Rolls-Royce Trent 900 TLM T-TRENT-9RR Revision 68 dated 24 February 2025.
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 24 March 2025.
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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