Safety Publications Tool
2017-0063 : Fuselage – Frame 40 Skin Panel Junction – Inspection
EASA approval number
EASA Large Transport Aeroplanes Section
/ Type Designation
This AD supersedes EASA AD 2014-0136 dated 13 June 2014.
Publication(s) and related information
Airbus SB A330-53-3215 original issue dated 21 June 2013, or Revision 01 dated 17 April 2014, or Revision 02 dated 23 November 2016; Airbus SB A340-53-4215 original issue dated 21 June 2013, or Revision 01 dated 17 April 2014, or Revision 02 dated 23 November 2016. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 24 January 2017 as PAD 17-012 for consultation until 21 February 2017. The Comment Response Document 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[dot]europa.eu.
EASA_AD_2017_0063.pdf (347 kb)
EASA_PAD_17_012.zip (933 kb)
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