Number |
2024-0068 |
Issued by |
Europe |
Issue date |
2024-03-11 |
Effective date |
2024-03-25 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
A318-111
-
A318-112
-
A318-121
-
A318-122
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
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 2022-0151 dated 26 July 2022.
|
Publication(s) and related information |
Airbus SB A320-53-1410 original issue dated 05 June 2018, or Revision 01 dated 26 January 2022, or Revision 02 dated 19 October 2022, or Revision 03 dated 29 May 2023.
Airbus SB A320-53-1411 original issue dated 05 June 2018, or Revision 01 dated 26 January 2022, or Revision 02 dated 19 September 2022.
Airbus SB A320-53-1335 original issue dated 12 March 2019, or Revision 01 dated 04 November 2022.
Airbus SB A320-53-1336 original issue dated 12 March 2019, or Revision 01 dated 04 November 2022.
Airbus SB A320-53-1337 original issue dated 05 June 2018, or Revision 01 dated 24 June 2020.
Airbus SB A320-53-1338 original issue dated 05 June 2018, or Revision 01 dated 24 June 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
23-128 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 November 2023 as PAD 23-128 for consultation until 20 December 2023. No comments were received during the consultation period.
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.
|