| Number |
2012-0103 |
| Issued by |
 Europe |
| Issue date |
2012-06-19 |
| Effective date |
2012-06-25 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
-
A300F4-622R
|
| Revision |
Not applicable
|
| Correction |
This AD has been republished to correct Note 2 in Appendix 1.
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A300-53-6111 Revision 04 dated 25 August 2011.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Airbus Repair Instructions R53810322, R53810323, R53810329, R53810330, R53810331 and R53810332. |
| PAD number |
12-028 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 10 April 2012 as PAD 12-028 for consultation until 08 May 2012. 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[dot]eu.
|
