Number |
2024-0087 |
Issued by |
Europe |
Issue date |
2024-05-14 |
Effective date |
2024-04-30 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
57 |
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 Table 1 of this AD.
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A57R023-24 (including Appendix 1, SFTOG per MSN) original issue dated 21 February 2024, or Revision 1 dated 05 March 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
PAD number |
24-032 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 08 March 2024 as PAD 24-032 for consultation until 05 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.
|