| Number |
2016-0217 |
| Issued by |
 Europe |
| Issue date |
2016-11-02 |
| Effective date |
2016-11-16 |
| 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2014-0124R1 dated 23 June 2015 (the requirements applicable to A310 aeroplanes).
|
| Publication(s) and related information |
A310 ALS Part 2 Revision 01 dated 07 August 2015.
A310 ALS Part 2 Variation 1.1 dated 25 January 2016.
A310 ALS Part 2 Variation 1.2 dated 22 July 2016.
The use of later approved revisions or variations of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-101R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 14 July 2016 as PAD 16-101 for consultation until 11 August 2016 and republished on 11 August 2016 as PAD 16-101R1 for consultation until 25 August 2016. The Comment Response Documents can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
