Document ID: chunk:federal_register_of_legislation:F2006B02536:body:0:p2
Version: federal_register_of_legislation:F2006B02536
Segment Type: other
Provision Reference: 
Character Range: 2742–3546

on the left hand upper longeron and upper diagonal support tubes where they intersect on the left side of the fuselage frame just forward of the vertical fin front spar attachment point, on Model AT-602 aircraft. The cracks were found by the pilot and/or ground crew when they noticed excessive movement of the empennage due to the loss of torsional rigidity.

            Amendment 1 is issued in response to a new FAA AD, which changes the compliance times, and incorporates new and revised manufacturer service information that contains a terminating action for the repetitive inspection requirement.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 20 August 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 8 September 2004.