Number |
2014-0016R6 |
Issued by |
Europe |
Issue date |
2018-09-04 |
Effective date |
2018-09-04 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
57 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A380
-
A380-841
-
A380-842
-
A380-861
|
Revision |
This AD revises EASA AD 2014-0016R5 dated 13 October 2017.
|
Correction |
Not applicable
|
Supersedure |
The original issue of this AD superseded EASA AD 2012-0153 dated 23 August 2012.
|
Publication(s) and related information |
Airbus AOT A57R001-12 original issue dated 14 May 2012.
Airbus SB A380-57-8071 original issue dated 18 June 2013.
Airbus SB A380-57-8087 original issue dated 28 November 2013.
Airbus SB A380-57-8089 original issue dated 01 October 2014.
Airbus SB A380-57-8108 original issue dated 05 October 2015.
Airbus SB A380-57-8109 original issue dated 11 February 2016.
Airbus SB A380-57-8110 original issue dated 01 October 2015.
Airbus SB A380-57-8131 original issue dated 15 March 2016.
Airbus SB A380-57-8134 original issue dated 04 August 2016.
Airbus SB A380-57-8135 original issue dated 04 August 2016.
Airbus SB A380-57-8143 original issue dated 17 October 2016.
Airbus SB A380-57-8180 original issue dated 06 September 2017.
Airbus SB A380-57-8191 original issue dated 28 March 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
|
PAD number |
13-188 |
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 20 December 2013 as PAD 13-188 for consultation until 10 January 2014. 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.
|