Document ID: chunk:federal_register_of_legislation:F2016L01940:body:0:p2
Version: federal_register_of_legislation:F2016L01940
Segment Type: other
Provision Reference: 
Character Range: 2795–3502

severe internal corrosion of wing struts at the upper cuff fairing screw attachment hole area.
                Amendment 8 aligned this AD with the requirements of a new state of design FAA AD which supersedes AD 93-10-06; which was referenced in Amendment 7 of this AD.
                This Amendment 9 accepts and aligns to the requirements of FAA AD 2015-08-04 now that the USA is not the State of design. CASR Part 39 foreign state-of design requirements may not provide for automatic acceptance of the FAA AD. References to alternative X-Ray inspection have been removed and any AMOC application will be assessed by the CASA.

Ben Wilson
Delegate of the Civil Aviation Safety Authority
12 December 2016