| Number |
2022-0235 |
| Issued by |
 Europe |
| Issue date |
2022-12-01 |
| Effective date |
2022-12-15 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
-
RB211-535
-
RB211-535E4-37
-
RB211-535E4-B-37
-
RB211-535E4-C-37
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2012-0265 and AD 2012-0266, both dated 18 December 2012, AD 2014-0249R1 dated 18 February 2015 and AD 2015-0148 dated 24 July 2015. This AD also supersedes CAA UK AD 006-05-2001 dated May 2001 and AD G-2003-0007 dated 25 November 2003.
|
| Publication(s) and related information |
Rolls-Royce RB211-535E4 TLM T-211(535)-6RR revision 56 dated 01 May 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
22-140 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 24 October 2022 as PAD 22-140 for consultation until 21 November
2022. 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.
|
