| Number |
F-2001-265R2 |
| Issued by |
France |
| Issue date |
2002-11-23 |
| Effective date |
2002-11-23 |
| EASA approval number |
|
| ATA Chapter |
|
Approval Holder / Type Designation |
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| Revision |
This Revision 2 replaces AD 2001-265(B) R1 dated December 12, 2001. The aim of Revision 2 of this AD is to refer to the SB A310-34-2154 R4 and SB A300-34-6141 R2. Those revised SB are issued in order to enlarge the holes for the installation of SEXTANT Pitot probes (the application of previous issues of those SB required an AIRBUS repair solution to apply).
|
| Correction |
Not applicable
|
| Supersedure |
This Revision 2 replaces AD 2001-265(B) R1 dated December 12, 2001.
|
| Publication(s) and related information |
AIRBUS Service Bulletins:A300-34-0166, A310-34-2137 Revision 2, A310-34-2154 Revision 4, A300-34-6116 Revision 2, and A300-34-6141 Revision 2. (Any later approved revision of these SBs 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
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