| Number |
F-2001-133R3 |
| Issued by |
 Europe |
| Issue date |
2004-07-07 |
| Effective date |
2004-07-17 |
| EASA approval number |
2004-7035 |
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
|
| Revision |
Revision 3 requires the installation of this new axis (referenced 2734-0212007). The limit life value of this new axis was 1,000 flight hours. Furthermore, while waiting for complementary test results, these axis must be inspected every 100 hours.
|
| Correction |
Not applicable
|
| Supersedure |
This AD replaces DGAC France AD 2001-133R2 dated 24 December 2002.
|
| Publication(s) and related information |
APEX AIRCRAFT Service Bulletin No. 980901 Revision 4 dated June 2004. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
