Number |
2024-0097 |
Issued by |
Europe |
Issue date |
2024-05-02 |
Effective date |
2024-05-16 |
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
-
A319-151N
-
A319-153N
-
A319-171N
-
A320
-
A320-211
-
A320-212
-
A320-214
-
A320-215
-
A320-216
-
A320-231
-
A320-232
-
A320-233
-
A320-251N
-
A320-252N
-
A320-253N
-
A320-271N
-
A320-272N
-
A320-273N
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
-
A321-251N
-
A321-251NX
-
A321-252N
-
A321-252NX
-
A321-253N
-
A321-253NX
-
A321-271N
-
A321-271NX
-
A321-272N
-
A321-272NX
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2012-0118 dated 04 July 2012.
|
Publication(s) and related information |
Airbus SB A320-53-1195 Revision 03 dated 08 November 2011, or Revision 04 dated 22 August 2012, or Revision 05 dated 22 November 2013, or Revision 06 dated 29 August 2014, or Revision 07 dated 28 July 2016, or Revision 08 dated 27 September 2017, or Revision 09 dated 23 October 2018, or Revision 10 dated 11 June 2021, or Revision 11 dated 08 November 2023.
Airbus SB A320-53-1196 Revision 02 dated 08 November 2011, or Revision 03 dated 22 August 2012, or Revision 04 dated 22 November 2013, or Revision 05 dated 29 August 2014, or Revision 06 dated 28 July 2016, or Revision 07 dated 27 September 2017, or Revision 08 dated 23 October 2018, or Revision 09 dated 17 December 2020, or Revision 10 dated 08 November 2023.
Airbus SB A320-53-1325 Revision 04 dated 07 November 2023.
Airbus SB A320-53-1326 Revision 03 dated 07 November 2023.
Airbus SB A320-53-1502 original issue dated 07 November 2023.
Airbus SB A320-53-1503 original issue dated 07 November 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
24-035 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 19 March 2024 as PAD 24-035 for consultation until 16 April 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.
|