Number |
2021-0251R1 |
Issued by |
Europe |
Issue date |
2022-10-12 |
Effective date |
2022-10-19 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
-
A340-541
-
A340-542
-
A340-642
-
A340-643
|
Revision |
This AD revises EASA AD 2021-0251 dated 17 November 2021.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2019-0048 dated 11 March 2019 and EASA AD 2021-0068 dated 11 March 2021.
|
Publication(s) and related information |
Airbus A340 ALS Part 4 Revision 7 dated 01 July 2021.
The use of later approved revisions or variations of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
21-154 |
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 15 October 2021 as PAD 21-154 for consultation until 12 November 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.
|