| Number |
F-2004-118R1 |
| Issued by |
 Europe |
| Issue date |
2004-10-13 |
| Effective date |
2004-10-23 |
| EASA approval number |
2004-10125 |
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises DGAC AD F-2004-118 original issue, EASA Approval Number 2004-7517. The aim of this Revision 1 is to precise the grace period for the aircraft which have exceeded the thresholds (10 years or 12,000 Flight Cycles (FC) since the first flight of the aircraft) after the AD effective date.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC AD F-2004-118 original issue
|
| Publication(s) and related information |
Airbus Service Bulletins A330-55-3032 and A340-55-4029, as applicable to type (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
|
