Document ID: chunk:federal_register_of_legislation:F2009L02072:body:0:p2
Version: federal_register_of_legislation:F2009L02072
Segment Type: other
Provision Reference: 
Character Range: 3045–3736

Complete failure of these drag links could result in gear collapse during landing.

             Amendment 1 was published in response to a new EASA AD, which was prompted when a recent investigation of a new occurrence of cracking revealed that the replacement nose landing gear right hand upper drag link part number 532.20.12.289 had also suffered fatigue cracking, but in a different place.

             Amendment 2 is issued to correct an administrative error in the issue of the previous amendment which prevented it taking effect on the required date.  There is no change to the technical requirements.

David Villiers
Delegate of the Civil Aviation Safety Authority

22 May 2009