Number |
2011-0085R1 |
Issued by |
Europe |
Issue date |
2012-07-20 |
Effective date |
2012-08-01 |
EASA approval number |
|
ATA Chapter |
52 |
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 |
This AD revises EASA AD 2011-0085 dated 12 May 2011, including the
Correction dated 31 May 2011.
|
Correction |
This AD is corrected to highlight the connection between the aeroplanes
affected by the MOD 04439 and the consolidated MOD 04799.
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A310-52-2067 Original Issue or Revision 01 or Revision 02, and
Airbus SB A300-52-6065 Original Issue or Revision 01 or Revision 02.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
11-011 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 01 February 2011 as PAD
11-011 for consultation until 01 March 2011. The Comment Response
Document can be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|