| Number |
2019-0101R1 |
| Issued by |
 Europe |
| Issue date |
2020-08-20 |
| Effective date |
2020-08-27 |
| EASA approval number |
|
| ATA Chapter |
71 |
Approval Holder
/ Type Designation |
-
ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG
|
| Revision |
This AD revises EASA AD 2019-0101 dated 08 May 2019.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2018-0185 dated 29 August 2018.
|
| Publication(s) and related information |
Rolls-Royce NMSB RB.211-71-AJ576 original issue dated 17 March 2017, or Revision 1 dated 11 July 2018, or Revision 2 dated 05 April 2019.
Rolls-Royce SB RB.211-72-H499 original issue dated 16 October 2013.
Rolls-Royce SB RB.211-79-H640 original issue dated 16 October 2013, or Revision 1 dated 19 June 2014.
Rolls-Royce Alert SB RB.211-72-AK047 original issue dated 16 October 2018, or Revision 1 dated 01 April 2020, or Revision 2 dated 17 August 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
19-062 |
| 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 12 April 2019 as PAD 19-062 for consultation until 26 April 2019. 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.
|
