AD/PA-38/2 Aft Fuselage/Tailcone Area Modification 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/PA-38/2.

Piper PA-38 (Tomahawk) Series Aeroplanes

AD/PA-38/2 Aft Fuselage/Tailcone Area - Modification 13/2008

Requirement:	CANCELLED.
This AD is cancelled on 18 December 2008.
Background:	This unique Australian AD specified removal of incorrect rivets from the aft fuselage and tailcone area, and replacement by the correct rivets in accordance with Piper SB No. 600A.  Compliance was required before initial issue of a certificate of airworthiness.  The AD is no longer required.

David Villiers
Delegate of the Civil Aviation Safety Authority

5 November 2008