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|
| Number |
23-084R2 |
| Issued by |
 Europe |
| Issue date |
2023-09-21 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-A
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Trent 1000-A2
-
Trent 1000-AE
-
Trent 1000-AE2
-
Trent 1000-C
-
Trent 1000-C2
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Trent 1000-CE
-
Trent 1000-CE2
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Trent 1000-D
-
Trent 1000-D2
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Trent 1000-E
-
Trent 1000-E2
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Trent 1000-G
-
Trent 1000-G2
-
Trent 1000-H
-
Trent 1000-H2
-
Trent 1000-J2
-
Trent 1000-K2
-
Trent 1000-L2
|
| Revision |
This PAD is revised to expand the Applicability, proposing to require a one-time inspection of all affected parts, and, depending on findings, replacement.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce TRENT 1000 Alert NMSB 72-AK965 original issue dated 19 May 2023 and Revision 1 dated 01 August 2023.
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 October 2023.
2. This PAD was initially posted on 07 July 2023 as PAD 23-084 for consultation until 21 July 2023, and re-published on 31 August 2023 as PAD 23-084R1 for additional consultation until 14 September 2023. Both Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this PAD.
3. Enquiries regarding this PAD 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 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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