| Number |
2021-0262 |
| Issued by |
 Europe |
| Issue date |
2021-12-13 |
| Effective date |
2021-12-27 |
| EASA approval number |
|
| 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 PAD is revised in order to include in the ALS definition the recently published ALS Part 2 Revision 04 Issue 2 and Variation 4.1.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2016-0152R1 dated 26 March 2018.
|
| Publication(s) and related information |
Airbus A340 ALS Part 2 Revision 04 Issue 2 dated 10 November 2021.
Airbus A340 ALS Part 2 Variation 4.1 dated 02 November 2021.
The use of later approved variations or revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-149R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 14 October 2021 as PAD 21-149 for consultation until 11 November 2021 and republished as PAD 21-149R1 on 22 November 2021 for additional consultation until 06 December 2021. 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 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.
|
