| Number |
F-2003-368R2 |
| Issued by |
 Europe |
| Issue date |
2004-03-03 |
| Effective date |
2004-03-13 |
| EASA approval number |
2004-1614 |
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
-
DAHER AEROSPACE
-
TB
-
TB 10
-
TB 20
-
TB 200
-
TB 21
-
TB 9
|
| Revision |
This AD revises DGAC AD 2003-368 R1. The purpose of this Revision 2 is to exclude from aircraft effectivity, the ones being modified according to change n° MOD 10-0209-27 or Service Bulletin (SB) n° BS 10-140 which brings a definite solution to the problem.
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC AD 2003-368 R1.
|
| Publication(s) and related information |
EADS SOCATA Service Bulletin TB n° 10-130 Rev. 2 dated January, 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
|
