Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
26-120 |
| Issued by |
 Europe |
| Issue date |
2026-10-06 |
| EASA approval number |
|
| ATA Chapter |
24 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A350-24-P028 original issue dated 16 December 2019.
Airbus SB A350-24-P046 original issue dated 31 January 2019.
Airbus SB A350-24-P165 original issue dated 05 June 2026.
Airbus SB A350-24-P166 original issue dated 05 June 2026.
Airbus SB A350-24-P167 original issue, dated 05 June 2026, or Revision 01 dated 01 August 2026.
Airbus SB A350-24-P168 original issue dated 05 June 2026.
Airbus SB A350-24-P169 original issue dated 05 June 2026.
Airbus SB A350-24-P170 original issue dated 05 June 2026.
Airbus SB A350-24-P171 original issue dated 05 June 2026.
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 03 November 2026.
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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