Number |
2021-0183R1 |
Issued by |
Europe |
Issue date |
2021-09-20 |
Effective date |
2021-09-27 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
25 |
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 |
This AD revises EASA AD 2021-0183 dated 04 August 2021.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A320-25-1BVS original issue dated 18 December 2020.
Airbus SB A320-25-1BVT original issue dated 18 December 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
21-005 |
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 29 January 2021 as PAD 21-005 for consultation
until 26 February 2021. 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.
|