Number |
2016-0146R2 |
Issued by |
Europe |
Issue date |
2021-06-14 |
Effective date |
2021-06-14 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A321
-
A321-111
-
A321-112
-
A321-131
-
A321-211
-
A321-212
-
A321-213
-
A321-231
-
A321-232
|
Revision |
This AD revises EASA AD 2016-0146R1 dated 26 July 2018.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A320-53-1308 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1309 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1310 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1311 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1312 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1313 original issue dated 04 November 2015, or Revision 01 dated 12 March 2019.
Airbus SB A320-53-1345 original issue dated 23 November 2017, or Revision 01 dated 28 January 2021.
Airbus SB A320-53-1346 original issue dated 23 November 2017, or Revision 01 dated 28 January 2021.
Airbus SB A320-53-1347 original issue dated 23 November 2017.
Airbus SB A320-53-1348 original issue dated 23 November 2017, or Revision 01 dated 28 January 2021.
Airbus SB A320-53-1349 original issue dated 23 November 2017, or Revision 01, dated 31 May 2019.
Airbus SB A320-53-1350 original issue dated 23 November 2017.
Airbus SB A320-53-1427 original issue dated 05 July 2019.
Airbus SB A320-53-1428 original issue dated 05 July 2019.
Airbus SB A320-53-1429 original issue dated 05 July 2019.
Airbus SB A320-53-1430 original issue dated 05 July 2019.
Airbus SB A320-53-1431 original issue dated 05 July 2019.
Airbus SB A320-53-1432 original issue dated 05 July 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
16-083 |
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 01 June 2016 as PAD 16-083 for consultation until 15 June 2016. 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.
|