Number |
2022-0111R1 |
Issued by |
Europe |
Issue date |
2023-07-26 |
Effective date |
2023-08-02 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
57 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A319
-
A320
-
A320-214
-
A320-216
-
A320-232
-
A320-251N
-
A320-271N
-
A321
-
A321-211
-
A321-213
-
A321-231
-
A321-251N
-
A321-251NX
-
A321-252NX
-
A321-253N
-
A321-253NX
-
A321-271N
-
A321-271NX
-
A321-272N
|
Revision |
This AD revises EASA AD 2022-0111 dated 15 June 2022.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2019-0233 dated 18 September 2019, including its Correction dated 19 September 2019.
|
Publication(s) and related information |
Airbus AOT A57N012-19 original issue dated 20 March 2019, or Revision 01 dated 18 April 2019.
Airbus SB A320-57-1234 original issue dated 13 December 2021.
Airbus SB A320-57-1235 original issue dated 13 December 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
22-054 |
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 11 May 2022 as PAD 22-054 for consultation until 08
June 2022. 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.
|