| Number |
2009-0188 |
| Issued by |
 Europe |
| Issue date |
2009-08-26 |
| Effective date |
2009-09-09 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-601
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A300-53-6161 Original Issue or Revision 1.
Structural Repair Manual task 51-40-41.
Non Destructive Test Manual (NTM) task 51-10-01, Page Block 601, procedure A.
The use of later approved revisions of these documents is acceptable for
compliance with requirements of this AD. |
| PAD number |
09-066R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative
Methods of Compliance for this AD.
2. This AD was initially posted on 11 May 2009 as PAD 09-066 for
consultation until 01 June 2009. The Comment Response Document can
be found at https://ad.easa.europa.eu.
Subsequently, the PAD was revised and posted on 04 August 2009 as PAD
09-066R1 for consultation until 18 August 2009. No comments were
received during the additional 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, facsimile: + 33 5 61 93 44 51.
|
