Safety Publications Tool
2010-0185-E : SUPERSEDED BY EASA AD 2011-0135
EASA approval number
EASA General Aviation Section
/ Type Designation
BLANIK AIRCRAFT CZ
This AD supersedes EASA AD 2010-0160-E which superseded EASA AD 2010- 0122-E which superseded EASA AD 2010-0119-E dated 18 June 2010.
Publication(s) and related information
Aircraft Industries a.s. Mandatory Bulletin No. L13/109a “Checking of the connection of the bottom wing suspension with spar cap – review of the operation conditions”, issue 1 dated 18 June 2010. 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 safety assessment has requested not to implement the full consultation process and an immediate publication and notification. 3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Research Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
easa_ad_2010_0185_E_Superseded.pdf (225 kb)
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