| Number |
F-2002-639R1 |
| Issued by |
 Europe |
| Issue date |
2005-03-30 |
| Effective date |
2005-04-09 |
| EASA approval number |
2005-2578 |
| 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
-
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 DGAC France AD 2002-639 dated 24 December 2002, to reduce the Applicability of the AD.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded DGAC France AD 2001-071(B) and AD 2000-001-300(B)R1, which were also cancelled by their R1 and R2, respectively, both dated 24 December 2002.
|
| Publication(s) and related information |
AIRBUS Service Bulletin (SB) A300-53-0354 Revision 2, SB A300-53-0356, SB A300-53-0357, SB A310-53-2112 and SB A300-53-6129 Revision 2. Any later approved revision of these SB's is acceptable. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
