Safety Publications Tool
2013-0258 : Fuselage – Fuselage Frames and Ribs – Inspection / Repair
EASA approval number
EASA General Aviation Section
/ Type Designation
This AD supersedes DGAC France AD 85-21-(A) dated 27 February 1985.
Publication(s) and related information
SN Centrair SB 101-06 rev 1 dated 5 August 2013. 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. This AD was posted on 11 September 2013 as PAD 13-139 for consultation until 09 October 2013. 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_ad_2013_0258.pdf (215 kb)
easa_pad_13_139.zip (234 kb)
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