Number |
2024-0128 |
Issued by |
Europe |
Issue date |
2024-07-03 |
Effective date |
2024-07-17 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2016-0105R2 dated 08 October 2021.
|
Publication(s) and related information |
Airbus SB A320-53-1317 original issue dated 15 December 2015, or Revision 01 dated 19 June 2018, or Revision 02 dated 12 April 2024.
Airbus SB A320-53-1318 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018, or Revision 02 dated 12 April 2024.
Airbus SB A320-53-1319 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018, or Revision 02 dated 12 April 2024.
Airbus SB A320-53-1320 original issue dated 09 October 2015, or Revision 01 dated 18 June 2018, or Revision 02 dated 12 April 2024.
Airbus SB A320-53-1351 original issue dated 20 December 2017, or Revision 01 dated 23 July 2021.
Airbus SB A320-53-1352 original issue dated 20 December 2017, or Revision 01 dated 04 August 2021.
Airbus SB A320-53-1353 original issue dated 20 December 2017, or Revision 01 dated 23 June 2021.
Airbus SB A320-53-1354 original issue dated 20 December 2017, or Revision 01 dated 23 July 2021.
Airbus SB A320-53-1433 original issue dated 28 June 2019.
Airbus SB A320-53-1434 original issue dated 28 June 2019.
Airbus SB A320-53-1435 original issue dated 28 June 2019.
Airbus SB A320-53-1436 original issue dated 28 June 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
24-063 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 31 May 2024 as PAD 24-063 for consultation until 28 June 2024. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed ('zipped') file, attached to the record for this AD.
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.
|