| Number |
2016-0218 |
| 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.
-
A300-600
-
A300B4-601
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
-
A300F4-622R
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2006-0257 dated 24 August 2006 and EASA AD 2014-0124R1 dated 23 June 2015 (the requirements applicable to A300-600 aeroplanes).
|
| Publication(s) and related information |
A300-600 ALS Part 2 Revision 01 dated 07 August 2015.
A300-600 ALS Part 2 Variation 1.1 dated 25 January 2016.
A300-600 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 |
16-102R1 |
| 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 16-102 for consultation until 11 August 2016 and republished on 11 August 2016 as PAD 16-102R1 for consultation until 25 August 2016. The Comment Response Document 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.
|
