| Number |
2020-0218 |
| Issued by |
 Europe |
| Issue date |
2020-10-12 |
| Effective date |
2020-10-26 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A319
-
A319-111
-
A319-112
-
A319-113
-
A319-114
-
A319-115
-
A319-131
-
A319-132
-
A319-133
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A320-53-1211 original issue dated 18 July 2007, or Revision 01 dated 28 January 2008.
Airbus SB A320-53-1219 original issue dated 06 April 2009, or Revision 01 dated 16 March 2010, or Revision 02 dated 13 August 2010, or Revision 03 dated 18 July 2011, or Revision 04 dated 31 January 2012, or Revision 05 dated 03 July 2012.
Airbus SB A320-53-1301 original issue dated 01 February 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-045 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 27 February 2020 as PAD 20-045 for consultation until 26 March 2020. 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 Programming and Continued Airworthiness 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.
|
