Safety Publications Tool
18-014 : Fuselage – Side Box Beam Flange in Frame 43 Area – Inspection / Repair / Modification
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EASA approval number
EASA Large Transport Aeroplanes Section
/ Type Designation
This AD supersedes EASA AD 2013-0261 dated 28 October 2013.
Publication(s) and related information
Airbus SB A320-53-1258 original issue dated 18 October 2012, or Rev. 01 dated 27 June 2016, or Rev. 02 dated 07 September 2016. Airbus SB A320-53-1251 original issue dated 16 November 2012, or Rev. 01 dated 18 October 2013, or Rev. 02 dated 11 February 2016, or Rev. 03 dated 19 September 2016. Airbus A318/A319/A320/A321 ALS Part 2 Rev. 06 dated 10 April 2017. The use of later approved revisions of the above mentioned documents is acceptable for compliance with the requirements of this AD.
1. This Proposed AD will be closed for consultation on 02 March 2018. 2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
EASA_PAD_18_014.pdf (510 kb)
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