Number |
2016-0035R1 |
Issued by |
Europe |
Issue date |
2018-09-21 |
Effective date |
2018-10-19 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
|
Revision |
This AD revises EASA AD 2016-0035 dated 24 February 2016.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus SB A340-53-4065 original issue dated 15 May 1996, or Revision 01 dated 27 May 1998, or Revision 02 dated 22 February 1999, or Revision 03 dated 15 November 1999, or Revision 04 dated 01 June 2012.
Airbus SB A340-53-4135 original issue dated 12 July 2002, or Revision 01 dated 19 March 2003, or Revision 02 dated 21 June 2010, or Revision 03 dated 17 July 2012.
Airbus SB A340-53-4191 original issue dated 25 June 2012.
Airbus SB A340-53-4194 original issue dated 04 October 2012, or Revision 01 dated 16 August 2016.
Airbus SB A340-53-4196 original issue dated 16 May 2013.
Airbus SB A340-53-4197 original issue dated 16 May 2013.
Airbus SB A340-53-4198 original issue dated 24 May 2013, or Revision 01 dated 12 October 2016.
Airbus SB A340-53-4234 original issue dated 30 November 2015.
Airbus SB A340-53-4237 original issue dated 05 February 2018.
Airbus SB A340-53-4241 original issue dated 05 July 2018.
Airbus SB A340-53-4242 original issue dated 21 June 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
Airbus OIT 999-0133/14 Revision 02, dated 27 August 2015, provides additional information on the subject addressed by this AD. |
PAD number |
15-154 |
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 16 December 2015 as PAD 15-154. Revision 1 of this AD was posted on 20 July 2018 as PAD 18-104 for consultation on 03 August 2018. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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 PAD, can be reported to the EU aviation safety reporting system.
|