Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
Number |
24-076 |
Issued by |
Europe |
Issue date |
2024-07-02 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
57 |
Approval Holder / Type Designation |
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2022-0250 dated 14 December 2022.
|
Publication(s) and related information |
Airbus SB A350-57-P067 original issue dated 17 September 2020.
Airbus SB A350-57-P070 original issue dated 28 July 2021 or Revision 01 dated 14 March 2022.
Airbus SB A350-57-P072 original issue dated 24 June 2022.
Airbus SB A350-57-P073 original issue dated 24 June 2022.
Airbus SB A350-57-P074 original issue dated 24 June 2022.
Airbus SB A350-57-P091 original issue dated 30 May 2024.
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 30 July 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.
|