| Number |
2019-0286R1 |
| Issued by |
 Europe |
| Issue date |
2024-07-03 |
| Effective date |
2024-07-10 |
| 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
-
Trent 1000-A2
-
Trent 1000-AE
-
Trent 1000-AE2
-
Trent 1000-C
-
Trent 1000-C2
-
Trent 1000-CE
-
Trent 1000-CE2
-
Trent 1000-D
-
Trent 1000-D2
-
Trent 1000-E
-
Trent 1000-E2
-
Trent 1000-G
-
Trent 1000-G2
-
Trent 1000-H
-
Trent 1000-H2
-
Trent 1000-J2
-
Trent 1000-K2
-
Trent 1000-L2
|
| Revision |
This AD revises EASA AD 2019-0286 dated 26 November 2019.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Alert NMSB TRENT 1000 72-AK294 original issue dated 16 July 2019, or Revision 1 dated 04 June 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-189 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 11 October 2019 as PAD 19-189 for consultation until 08 November 2019. 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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