Number |
2021-0206 |
Issued by |
Europe |
Issue date |
2021-09-15 |
Effective date |
2021-09-29 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2020-0091 dated 22 April 2020.
|
Publication(s) and related information |
Airbus A350 ALS Part 1 Revision 04 dated 14 September 2018 and Variation 4.3 dated 07 June 2019, or Revision 05 dated 29 May 2020, and Revision 06 dated 30 June 2021.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD. |
PAD number |
21-118 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 17 August 2021 as PAD 21-118 for consultation until 14 September
2021. 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.
|