| Number |
2007-0243R1 |
| Issued by |
 Europe |
| Issue date |
2023-06-21 |
| Effective date |
2023-07-05 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300-600
-
A300-600ST (Beluga)
-
A310
|
| Revision |
This AD revises EASA AD 2007-0243 dated 04 September 2007.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded DGAC France AD 1997-358-232(B)R1 dated March 22, 2000 and DGAC France AD 1999-007-019 R1 dated 24 January 2001.
|
| Publication(s) and related information |
Airbus SB A300-57-0232 original issue dated 09 September 1997, or Revision 1 dated 12 January 1998, or Revision 2 dated 21 February 2000.
Airbus SB A300-57-6079 original issue dated 09 September 1997, or Revision 1 dated 13 October 1997, or Revision 2 dated 12 January 1998, or Revision 3 dated 25 October 1999, or Revision 4 dated 21 February 2000.
Airbus SB A310-57-2075 original issue dated 09 September 1997, or Revision 1 dated 12 January 1998, or Revision 2 dated 21 February 2000, or Revision 3 dated 01 December 2006.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
07-132 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. The original issue of this AD was posted on 06 August 2007 as PAD 07-132 for consultation until 03 September 2007. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be
installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate
(STC) or other modification.
|
