AD/PA-34/35 Fuselage Structure, LH Side Sta.108 Inspection and 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-34/35.

Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/35 Fuselage Structure, LH Side
Sta.108 - Inspection and Modification 11/2008

Requirement:	CANCELLED.
This AD is cancelled on 23 October 2008.
Background:	This unique Australian AD specified a once-only inspection and modification of the fuselage structure in accordance with Piper SB No. 711.  Compliance was required within 100 hours time in service after May 1981.  The AD is no longer required.

David Villiers
Delegate of the Civil Aviation Safety Authority

9 September 2008