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|
Number |
23-029 |
Issued by |
Europe |
Issue date |
2023-03-01 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
35 |
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
-
A330
-
A330-201
-
A330-202
-
A330-203
-
A330-223
-
A330-223F
-
A330-243
-
A330-243F
-
A330-301
-
A330-302
-
A330-303
-
A330-321
-
A330-322
-
A330-323
-
A330-341
-
A330-342
-
A330-343
-
A330-841
-
A330-941
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
-
A340-541
-
A340-542
-
A340-642
-
A340-643
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus AOT A35N017-22 original issue dated 29 November 2022, or Revision 01 dated 19 January 2023, or Revision 02 dated 14 February 2023.
Airbus AOT A35L018-22 original issue dated 29 November 2022, or Revision 01 dated 19 January 2023, or Revision 02 dated 14 February 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. This Proposed AD will be closed for consultation on 29 March 2023.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred on a product, part or appliance not affected by this PAD, 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 PAD 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.
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