| Number |
2024-0079 |
| Issued by |
 Europe |
| Issue date |
2024-04-04 |
| Effective date |
2024-04-09 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
| Revision |
Not applicable
|
| Correction |
This AD is republished to correct a typographical error in its effective date.
|
| Supersedure |
This AD supersedes EASA AD 2023-0124 dated 16 June 2023.
|
| Publication(s) and related information |
Airbus AOT A32R026-22 original issue dated 27 April 2022, or Revision 01 dated 06 February 2023, or Revision 02 dated 22 March 2023, or Revision 03 dated 10 January 2024, or Revision 04 dated 15 February 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until 23 April 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.
|
