| Number |
F-2002-608R1 |
| Issued by |
France |
| Issue date |
2003-01-08 |
| Effective date |
2002-12-21 |
| EASA approval number |
|
| ATA Chapter |
27 |
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 and replaces DGAC France AD 2002-608(B) dated December 11, 2002, to clarify the thresholds defined in paragraph 3.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AIRBUS SB A300-27A0197, or SB A310-27A2098, or SB A300-27A6051, as applicable. Any later approved revisions of these SBs are 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
|