Number |
2024-0030 |
Issued by |
Europe |
Issue date |
2024-01-31 |
Effective date |
2024-02-14 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
05 |
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 2022-0091 dated 20 May 2022 and EASA AD 2023-0138 dated 13 July 2023.
|
Publication(s) and related information |
Airbus A318/A319/A320/A321 ALS Part 3 Revision 09 dated 06 November 2023, or ALS Part 3
Revision 09 Variation 9.1 dated 15 December 2023.
The use of later approved variations or revisions of the above-mentioned document is acceptable
for compliance with the requirements of this AD. |
PAD number |
23-143 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 14 December 2023 as PAD 23-143 for consultation until 11 January
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.
|