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ADs [at] easa.europa [dot] eu
|
Number |
24-041 |
Issued by |
Europe |
Issue date |
2024-04-09 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
28 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2021-0073 dated 15 March 2021.
|
Publication(s) and related information |
Airbus SB A380-28-8072 original issue dated 07 January 2021, or Revision 01 dated 10 May 2023, or Revision 02 dated 21 March 2024.
Airbus SB A380-28-8073 original issue dated 07 January 2021.
Airbus RDAF 81233570/016/2023 dated 12 June 2023.
Airbus RDAF 81233570/021/2023 dated 30 June 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
Remarks |
1. This Proposed AD will be closed for consultation on 07 May 2024.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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.
|