| Number |
2016-0241 |
| Issued by |
Europe |
| Issue date |
2016-12-06 |
| Effective date |
2016-12-20 |
| EASA approval number |
|
| ATA Chapter |
53 |
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
-
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 |
None
|
| Publication(s) and related information |
Airbus SB A310-53-2143 at original issue dated 11 February 2016.
Airbus SB A300-53-6185 at original issue dated 11 February 2016.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
16-109 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 July 2016 as PAD 16-109 for consultation until 19 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.
|