Safety Publications Tool
2013-0013R1 : Wings – Rear Spar Build Slot between Ribs 1 and 2 – Inspection
EASA approval number
EASA Large Aeroplane Section
/ Type Designation
This AD revises EASA AD 2013-0013 dated 15 January 2013, which superseded DGAC France AD 1997-375-239(B)R3 dated 12 July 2000.
Publication(s) and related information
Airbus SB A300-57-6059 Revision 04 dated 22 February 2011. The use of later approved revisions of this document 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. The original issue of this AD was posted on 26 November 2012 as PAD 12-148 for consultation until 24 December 2012. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
easa_pad_12_148.zip (947 kb)
easa_ad_2013_0013_R1.pdf (217 kb)
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