Document ID: chunk:federal_register_of_legislation:F2006B11061:body:0:p2
Version: federal_register_of_legislation:F2006B11061
Segment Type: other
Provision Reference: 
Character Range: 2771–3551

to correct the referenced requirements document from Service Bulletin No. 25 to Service Letter No.25.

            Amendment 1 was issued as a result of extensive corrosion being found in an elevator control push rod joint after it failed in flight. Corrosion was not evident from an external visual inspection because it affected the tails of the rivets attaching the end fitting to the tube.

            Initial issue of this Airworthiness Directive resulted from the Type Certificate holder advising of corrosion being found in critical structural elements of the aircraft.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 30 November 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 22 December 2004.