| Number |
2015-0176 |
| Issued by |
Europe |
| Issue date |
2015-08-25 |
| Effective date |
2015-09-08 |
| EASA approval number |
|
| ATA Chapter |
24 |
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
-
A300-600ST (Beluga)
-
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 2014-0034 dated 05 February 2014.
|
| Publication(s) and related information |
Airbus SB A300-24-6103 Revision 03 dated 03 July 2015.
Airbus SB A300-24-9014 Revision 02 dated 20 February 2015.
Airbus SB A310-24-2105 original issue dated 20 March 2013, or Revision 01
dated 11 December 2013, or Revision 02 dated 05 January 2015.
Airbus SBIT 14-0044 original issue dated 17 October 2014, or Revision 01
dated 06 February 2015.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
15-098 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 24 July 2015 as PAD 15-098 for consultation until
21 August 2015. No comments were received during the consultation
period.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|