Document ID: chunk:federal_register_of_legislation:F2006B04204:body:0:p2
Version: federal_register_of_legislation:F2006B04204
Segment Type: other
Provision Reference: 
Character Range: 2948–3726

modification before this time as terminating action for the repetitive inspection and retorque requirements.

            This Airworthiness Directive becomes effective on 28 October 2004.

            Background: This Directive is the result of numerous reports of loose bolts on the pedestal attachment of the throttle/prop cross shaft assembly. The requirements detailed in this Directive are to detect and correct loose bolts not securing the pedestal cross shaft, which could result in limited effectiveness of the control levers. This failure could lead to an aborted takeoff.

 James Coyne
 Delegate of the Civil Aviation Safety Authority 17 September 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 6 October 2004.