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ADs [at] easa.europa [dot] eu
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| Number |
24-106 |
| Issued by |
 Europe |
| Issue date |
2024-08-22 |
| EASA approval number |
|
| Contributor |
EASA Large Aeroplanes Department |
| ATA Chapter |
35 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2019-0168 dated 16 July 2019.
|
| Publication(s) and related information |
Airbus AOT A35P010-17 original issue dated 20 December 2018, Revision 01 dated 11 April 2019, or Revision 02 dated 28 October 2021.
Airbus SB A350-35-P019 original issue dated 08 February 2024, or Revision 01 dated 12 June 2024.
B/E Aerospace SB 4441227-35-003 dated 19 December 2017.
B/E Aerospace SB 4441227-35-004 dated 08 April 2019.
Collins Aerospace SB 4441227-35-005 dated 23 November 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 19 September 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.
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