Number |
2009-0189 |
Issued by |
Europe |
Issue date |
2009-08-26 |
Effective date |
2009-09-09 |
EASA approval number |
|
ATA Chapter |
78 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-103
-
A300B4-203
-
A300B4-2C
-
A300C4-203
-
A300F4-203
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD F-2005-206, EASA approval 2005-6432.
|
Publication(s) and related information |
Airbus SB A300-78-0021 original issue or Revision 01,
Airbus SB A300-78-0022 original issue or Revision 01, and
Airbus SB A300-54-0098 Revision 02.
The use of later approved revisions of these documents is acceptable for
compliance with requirements of this AD. |
PAD number |
09-021 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 29 July 2009 as PAD 09-021 for consultation
until 19 August 2009. No comments were received during the
consultation period.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA; E-mail ADs@easa.europa.eu.
4. For any question concerning the technical content of the requirements in
this AD, please contact: Airbus SAS – EAW (Airworthiness Office,
Telephone: + 33 5 61 93 36 96, Fax: + 33 5 61 93 44 51).
|