| Number |
2025-0072 |
| Issued by |
 Europe |
| Issue date |
2025-03-31 |
| Effective date |
2025-04-14 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 800
-
875-17
-
877-17
-
884-17
-
884B-17
-
892-17
-
892B-17
-
895-17
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes UK CAA AD G-2003-0003 dated 18 September 2003, including its Correction dated 25 November 2003, EASA AD 2007-0003R1 dated 15 January 2009, including its Correction dated 06 February 2009, EASA AD 2007-0004 dated 08 January 2007, EASA AD 2012-0051 dated 26 March 2012 and EASA AD 2016-0223 dated 08 November 2016.
|
| Publication(s) and related information |
Rolls-Royce RB211 Trent 800 engines TLM T-TRENT-2RR Revision 59 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 |
25-038 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 28 February 2025 as PAD 25-038 for consultation until 28 March 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.
|
