Number |
2013-0267R1 |
Issued by |
Europe |
Issue date |
2014-05-08 |
Effective date |
2014-03-11 |
EASA approval number |
|
Contributor |
EASA Large Aeroplanes Section |
ATA Chapter |
32 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A330
-
A330-201
-
A330-202
-
A330-203
-
A330-223
-
A330-223F
-
A330-243
-
A330-243F
-
A330-301
-
A330-302
-
A330-303
-
A330-321
-
A330-322
-
A330-323
-
A330-341
-
A330-342
-
A330-343
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
|
Revision |
This AD revises EASA AD 2013-0267 dated 06 November 2013, which superseded EASA AD 2012-0015 dated 23 January 2012.
|
Correction |
This AD is republished to editorially correct paragraph (4).
|
Supersedure |
The original issue of this AD superseded EASA AD 2012-0015 dated 23 January 2012.
|
Publication(s) and related information |
Airbus SB A330-32-3225 original issue dated 21 November 2007, or Revision 01 dated 30 October 2008, or Revision 02 dated 26 October 2012.
Airbus SB A340-32-4268 original issue dated 21 November 2007, or Revision 01 dated 30 October 2008, or Revision 02 dated 26 October 2012, or Revision 03 dated 14 January 2013.
Messier-Dowty SB N° A33/34-32-271 original issue dated 13 September 2007, or Revision 1 dated 16 November 2007.
Messier-Dowty SB N° A33/34-32-272 original issue dated 16 November 2007, or Revision 1 dated 22 September 2008.
Messier-Dowty SB N° A33/34-32-278 original issue dated 17 February 2010, or Revision 1 dated 24 August 2011.
Messier-Dowty SB N° A33/34-32-283 original issue dated 11 May 2010, or Revision 1 dated 10 July 2012.
Messier-Dowty SB N° A33/34-32-284 original issue dated 11 May 2010, or Revision 1 dated 10 July 2012.
Airbus SB A330-32-3237 original issue dated 18 January 2011, or Revision 01 dated 14 October 2011.
Airbus SB A340-32-4279 original issue dated 18 January 2011, or Revision 01 dated 14 October 2011.
Airbus SB A330-32-3222 original issue dated 10 January 2008.
Airbus SB A340-32-4265 original issue dated 11 January 2008.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.
|