| Number |
2007-0201R1 |
| Issued by |
 Europe |
| Issue date |
2025-10-16 |
| Effective date |
2025-10-23 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211 TRENT 700
-
768-60
-
772-60
-
772B-60
-
772C-60
|
| Revision |
This AD revises EASA AD 2007-0201 dated 01 August 2007.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2006-0355 dated 04 December 2006, which superseded CAA United Kingdom AD G-2004-0016 (EASA Approval 2004-6754), which superseded CAA-UK AD G-2003-0016 (EASA Approval 2003-1866).
|
| Publication(s) and related information |
RR Trent 700 Alert NMSB RB.211-72-AE302 Revision 5 dated 22 May 2007, or Revision 6 dated 29 January 2009, or Revision 7 dated 30 April 2009, or Revision 8 dated 21 October 2009, or Revision 9 dated 16 June 2010, or Revision 10 dated 02 February 2011, or Revision 11 dated 23 March 2021, or Revision 12 dated 30 June 2021, or Revision 13 dated 12 October 2022, or Revision 14 dated 06 November 2023.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
07-099 |
| 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 15 June 2007 as PAD 07-099 for consultation until 28 June 2007. 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.
|
