Number |
2021-0227 |
Issued by |
Europe |
Issue date |
2021-10-11 |
Effective date |
2021-10-25 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
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
-
A320
-
A320-211
-
A320-212
-
A320-214
-
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 |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A320-53-1373 original issue dated 14 June 2018.
Airbus SB A320-53-1374 original issue dated 14 June 2018.
Airbus SB A320-53-1378 original issue dated 14 June 2018, or Revision 01 dated 17 September
2019.
Airbus SB A320-53-1379 original issue dated 14 June 2018, or Revision 01 dated 17 September
2019, or Revision 02 dated 13 January 2021.
Airbus SB A320-53-1380 original issue dated 14 June 2018, or Revision 01 dated 13 September
2019.
Airbus SB A320-53-1381 original issue dated 14 June 2018, or Revision 01 dated 18 September
2019.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
21-113 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 04 August 2021 as PAD 21-113 for consultation until 01 September
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.
|