Number |
2022-0259 |
Issued by |
Europe |
Issue date |
2022-12-20 |
Effective date |
2023-01-03 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
TRENT 1000
-
Trent 1000-A
-
Trent 1000-AE
-
Trent 1000-C
-
Trent 1000-CE
-
Trent 1000-D
-
Trent 1000-E
-
Trent 1000-G
-
Trent 1000-H
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2020-0242 dated 05 November 2020.
|
Publication(s) and related information |
Rolls-Royce Trent 1000 TLM T-Trent-10RRB, Revision 28 dated 01 July 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
22-151 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 November 2022 as PAD 22-151 for consultation until 08 December 2022. 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.
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