| Number |
2013-0223R1 |
| Issued by |
 Europe |
| Issue date |
2020-09-30 |
| Effective date |
2020-10-07 |
| EASA approval number |
|
| ATA Chapter |
72 |
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 |
This AD revises EASA AD 2013-0223 dated 19 September 2013.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-72-AG644 original issue dated 30 April 2013, or Revision 1 dated 18 September 2014, or Revision 2 dated 28 April 2016, or Revision 3 dated 3 September 2020.
Rolls-Royce SB RB.211-72-G604 original issue dated 18 March 2013, or Revision 1 dated 28 January 2015, or Revision 2 dated 18 February 2016.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-084 & 13-084R1 |
| 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 19 June 2013 as PAD 13-084 and republished on 23 August 2013 as PAD 13-084R1 for consultation until 06 September 2013. 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 Programming and Continued Airworthiness 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.
|
