Document ID: chunk:federal_register_of_legislation:F2006B07107:body:0:p2
Version: federal_register_of_legislation:F2006B07107
Segment Type: other
Provision Reference: 
Character Range: 2825–3868

Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

2.    At 100 flying hour intervals.

3.    Prior to further flight.

            This Amendment becomes effective on 6 September 2001.

            Background:   The measures in this Directive resulted from investigation into an accident involving a SA330, which lost drive to the tail rotor due to worn splines on the bevel wheel and on the tail rotor drive shaft.

            This Amendment updates the reference SB revision status, revises the wear limits and compliance intervals.

            Amendment 1 clarified the applicability and compliance requirements. Amendment 1 of this Airworthiness Directive became effective on 20 May 1999.
            The original issue of this Airworthiness Directive became effective on 6 November 1997.

 Eugene Paul Holzapfel
 Delegate of the Civil Aviation Safety Authority 26 July 2001

 The above AD is notified in the Commonwealth of Australia Gazette on 15 August 2001.