| Number |
2020-0258 |
| Issued by |
 Europe |
| Issue date |
2020-11-19 |
| Effective date |
2020-12-02 |
| EASA approval number |
|
| ATA Chapter |
32 |
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
|
| Revision |
Not applicable
|
| Correction |
This AD has been republished to correct typographical errors in the Ref. Publications section.
|
| Supersedure |
This AD supersedes EASA AD 2018-0136 dated 26 June 2018.
|
| Publication(s) and related information |
Airbus SB A320-32-1461 original issue dated 11 April 2018.
Airbus AOT A32N022-20 original issue dated 15 October 2020, or Revision 01 dated 16 November 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
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.
|
