Number |
2020-0112R1 |
Issued by |
Europe |
Issue date |
2020-05-27 |
Effective date |
2020-06-03 |
EASA approval number |
|
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A310
-
A310-203
-
A310-203C
-
A310-204
-
A310-221
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
Revision |
This AD revises EASA AD 2020-0112 dated 20 May 2020.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus A310 ALS Part 2 Revision 03 Variation 3.2 dated 01 July 2019.
Airbus A310 ALS Part 2 Revision 03 Variation 3.3 dated 17 December 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
19-215 |
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 18 December 2019 as PAD 19-215 for consultation until 15 January 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.
|