Document ID: chunk:federal_register_of_legislation:F2006B02837:body:0:p2
Version: federal_register_of_legislation:F2006B02837
Segment Type: other
Provision Reference: 
Character Range: 2923–3531

before 15 March 2000.

            This Airworthiness Directive becomes effective on 8 February 2000.

            Background:  This AD is prompted by reports indicating numerous discrepancies in the installation of the fastener that connects the input rod of the spoiler mixer mechanism to the torque tube crank which could result in a disconnect and consequent reduced controllability of the aeroplane.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 7 February 2000

 The above AD is notified in the Commonwealth of Australia Gazette on 8 February 2000.