| Number |
F-2001-580R2 |
| Issued by |
 Europe |
| Issue date |
2004-12-08 |
| Effective date |
2004-12-18 |
| EASA approval number |
2004-11502 |
| ATA Chapter |
05, 67 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 B3
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
|
| Revision |
This AD revises DGAC France AD 2001-580-085 R1 dated 12 June 2002, to make reference to AS350 ASB No.05.00.37 Revision 1; and to MOD 073205 (offsetting the effective travel of the SAMM tail servocontrol following the increase in the yaw control range), and further information and Figure 2 added to the referenced ASB.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
EUROCOPTER AS 350 ASB No. 05.00.37 R1 (Any subsequent approved revision to this ASB 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
|
