| Number |
2025-0050 |
| Issued by |
 Europe |
| Issue date |
2025-02-26 |
| Effective date |
2025-03-12 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 500
-
RB211 Trent 553-61
-
RB211 Trent 553A2-61
-
RB211 Trent 556-61
-
RB211 Trent 556A2-61
-
RB211 Trent 560A2-61
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes UK CAA AD G-2003-0005 dated 25 November 2003, EASA AD 2008-0042 dated 27 February 2008 and EASA AD 2008-0098 dated 21 May 2008.
|
| Publication(s) and related information |
Rolls-Royce RB211 Trent 500 engines Time Limits Manual (TLM) T-TRENT-5RR Revision 52 dated 07 February 2025.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-033 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 11 February 2025 as PAD 25-033 for consultation until 25 February 2025. No comments were received during the consultation period.
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.
|
