| Number |
2017-0082 |
| Issued by |
 Europe |
| Issue date |
2017-05-08 |
| Effective date |
2017-05-22 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-102
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
A300B4-220
-
A300B4-2C
-
A300C4-203
-
A300F4-203
-
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 |
This AD supersedes EASA AD 2015-0238 dated 18 December 2015.
|
| Publication(s) and related information |
Airbus AOT A53W010-15 original issue dated 15 December 2015, and Revision 01 dated 04 October 2016.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
| PAD number |
17-027 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 March 2017 as PAD 17-027 for consultation until 04 April 2017. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
