AD/PT6A/15 Reversing Linkage Front End Clevis Incorporation of Inspection Hole Cancelled (Cth)

AIRWORTHINESS DIRECTIVE

On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive AD/PT6A/15.

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD/PT6A/15 Reversing Linkage Front End
Clevis - Incorporation of Inspection Hole 7/2009

Requirement:	CANCELLED.
This AD is cancelled on 2 July 2009.
Background:	This unique Australian AD specified action in accordance with UACL SB No. 166 or SB No. 1119 within 100 hours time in service after October 1974.  The AD is no longer required.

James Coyne
Delegate of the Civil Aviation Safety Authority

18 May 2009