2011-0135R1 : Prohibition of all flights / Restoration of Airworthiness Wings – Wing Main Spar – Inspection / Operational Limitation / Operational Records Check
EASA approval number
EASA General Aviation Section
/ Type Designation
This AD revises EASA AD 2011-0135 dated 20 July 2011 (including its Correction dated 18 November 2011), which superseded EASA Emergency AD 2010-0185-E dated 03 September 2010.
The original issue of this AD superseded EASA Emergency AD 2010-0185-E dated 03 September 2010.
Publication(s) and related information
AI IB No L13/107b, dated 18 July 2011. AI MB No L13/108a, dated 14 July 2011. AI MB No L13/112a, dated 16 May 2011. AI MB No L13/117a, dated 20 January 2016. Aircraft Design and Certification Ltd. modification ADxC-DC-39-001, approved by EASA through STC 10035295, which includes associated documentation: - ADxC-39-EO-013, Issue A, dated 01 April 11 (Template for installation of structural modification), - ADxC-39-001-AFM dated 30 March 11 (AFM supplement), and - ADxC-39-001-AMM dated 11 June 11 (MM supplement). 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. The required actions and the risk allowance have granted the issuance of a Final AD with Request for Comments, postponing the public consultation process after publication. 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_2011_0135_R1.pdf (363 kb)
easa_ad_2011_0135.zip (1 mb)
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