Ad/Bell 206/5 - Cyclic Pitch Control System Lever - 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/BELL 206/5.

Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

AD/BELL 206/5 Cyclic Pitch Control System
Lever - Inspection and Modification 11/2008

Requirement:	CANCELLED.
This AD is cancelled on 23 October 2008.
Background:	This unique Australian AD, issued in 1968, required inspection and modification of the cyclic control system lever assembly in accordance with Bell Alert Service Bulletin 206A-2 to ensure the forward cyclic movement was not restricted.  The AD compliance required inspection within 10 hours time in service and modification within 100 hours time in service from 6 June 1968.  As all aircraft would have been modified by now, the AD is no longer required.

James Coyne
Delegate of the Civil Aviation Safety Authority

25 August 2008