Number |
2017-0237R1 |
Issued by |
Europe |
Issue date |
2022-06-08 |
Effective date |
2022-06-22 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Department |
ATA Chapter |
27 |
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
-
A320-215
-
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 |
This AD revises EASA AD 2017-0237 dated 04 December 2017.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD supersedes EASA AD 2014-0147 dated 11 June 2014.
|
Publication(s) and related information |
Airbus SB A320-27-1245 original issue dated 06 March 2017, or Revision 01 dated 20 August 2018, or Revision 02 dated 22 July 2020.
Airbus SB A320-27-1246 original issue dated 20 March 2015, or Revision 01 dated 04 November 2016.
Airbus SB A320-27-1247 original issue dated 06 March 2017, or Revision 01 dated 28 June 2018, or Revision 02 dated 17 October 2019, or Revision 03 dated 28 October 2020.
Airbus SB A320-27-1248 original issue dated 06 March 2017, or Revision 01 dated 16 April 2018, or Revision 02 dated 20 September 2019, or Revision 03 dated 23 July 2020, or Revision 04 dated 12 November 2021, or Revision 05 dated 01 February 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
17-140 |
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 06 October 2017 as PAD 17-140 for consultation until 03 November 2017. 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.
|