Number |
2022-0120R2 |
Issued by |
Europe |
Issue date |
2023-07-28 |
Effective date |
2023-08-04 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
25 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A318
-
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 |
This AD revises EASA AD 2022-0120R1 dated 30 June 2022.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2021-0172 dated 20 July 2021.
|
Publication(s) and related information |
Airbus SB A320-25A1555 Revision 03 dated 28 February 2012.
Airbus SB A320-25-1557 original issue dated 14 June 2007, or Revision 01 dated 07 February 2008, or Revision 02 dated 05 November 2008, or Revision 03 dated 01 July 2013.
Airbus SB A320-53-1215 original issue dated 05 November 2008, or Revision 01 dated 26 July 2013.
Airbus SB A320-25-1BKJ Revision 02 dated 09 April 2020, or Revision 03 dated 17 February 2022, or Revision 04 dated 29 April 2022, or Revision 05 dated 30 May 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
|
PAD number |
22-030 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 22 March 2022 as PAD 22-030 for consultation until 19 April 2022. 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.
|