| Number |
2008-0052R1 |
| Issued by |
 Europe |
| Issue date |
2008-06-30 |
| Effective date |
2008-03-19 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300-600
-
A300-600ST (Beluga)
-
A310
|
| Revision |
AD 2008-0052 has been revised to take into account the various corrective measures resulting in specific inspection intervals and paragraph (1) of the Compliance section has been amended accordingly. In addition, paragraph (3) has been changed to correct the compliance time allowed for aircraft that have already exceeded the threshold for the initial torque check.
|
| Correction |
N/A
|
| Supersedure |
DGAC France AD F-2004-075, EASA approval number 2004-5338; and AD F-2004-076.
This AD revises and replaces EASA AD 2008-0052 dated 05 March 2008, including the Corrections thereof, dated 10 March 2008 and 12 March 2008.
|
| Publication(s) and related information |
AIRBUS AOT A300-32A0447 original issue; A310-32A2132 original issue; A300-32A6093 original issue; A300-32A9009 original issue;
AIRBUS Inspection Service Bulletin A300-32-0447 revision 1; A310-32-2132 revision 1; A300-32-6093 revision 1; A300-32-9009 revision 1.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
|
| PAD number |
07-171 |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
