| Number |
2024-0010 |
| Issued by |
 Europe |
| Issue date |
2024-01-09 |
| Effective date |
2024-01-23 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A310
-
A310-203
-
A310-203C
-
A310-204
-
A310-221
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2019-0091 dated 26 April 2019, EASA AD 2020-0112R1 dated 27 May 2020, EASA AD 2021-0205 dated 14 September 2021, EASA AD 2021-0257 dated 17 November 2021, EASA AD 2022-0193 dated 23 September 2022 and EASA AD 2023-0092 dated 05 May 2023.
|
| Publication(s) and related information |
Airbus A310 ALS Part 2 DT-ALI Revision 04 dated 20 July 2023.
The use of later approved variations or revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
23-139 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 05 December 2023 as PAD 23-139 for consultation until 02 January 2024. 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.
|
