Document ID: chunk:federal_register_of_legislation:F2005L02168:body:0:p2
Version: federal_register_of_legislation:F2005L02168
Segment Type: other
Provision Reference: 
Character Range: 2786–3527

the propeller.

             Exceeding the service life of the propeller could lead to failure of the hubs or blades resulting in subsequent loss of aeroplane control.

             Actions specified by this AD address the safety risk associated with the loss of aeroplane control.

             The current Amendment of this AD addresses an administrative omission in the earlier Amendment, with no change in technical content or the compliance schedule.

             Amendment 1 of this AD aligned the compliance statement to the FAA AD and became effective on 01 August 2005.

             The original issue of this AD became effective on 11 March 2003.

James Coyne
Delegate of the Civil Aviation Safety Authority

1 August 2005