| Number |
F-2005-084R1 |
| Issued by |
 Europe |
| Issue date |
2005-08-17 |
| Effective date |
2005-08-17 |
| EASA approval number |
2005-6142 |
| 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 |
This AD revises DGAC France AD F-2005-084 (EASA approval 2005-4320) dated 25 May 2005, including the Correction dated 08 June 2005.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AIRBUS SB A300-53-0365 original issue or Revision 1, SB A300-53-6138 original issue or Revision 1, SB A310-53-2117 original issue or Revision 1, SB A300-53-0364 original issue or Revision 1 or Revision 2, SB A300-53-6137 original issue or Revision 1 or Revision 2 or Revision 3, and/or SB A310-53-2116 original issue or Revision 1 or Revision 2, as applicable. Any later approved revisions 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
|
