| Number |
2020-0211 |
| Issued by |
 Europe |
| Issue date |
2020-10-05 |
| Effective date |
2020-10-19 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2017-0030 dated 15 February 2017.
|
| Publication(s) and related information |
Airbus A350 ALS Part 4 Revision 02 dated 24 June 2016, Revision 03 dated 15 December 2017, Revision 04 dated 14 September 2018, Revision 05 original issue dated 29 May 2020 and Revision 05 issue 2 dated 25 June 2020.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-137 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 09 September 2020 as PAD 20-137 for consultation until 23 September 2020. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs@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.
|
