AD/Bell 206/15 Tail Rotor Pedal Controls 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 206/15.

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

AD/BELL 206/15 Tail Rotor Pedal Controls Modification 11/2008

Requirement:	CANCELLED.
This AD is cancelled on 23 October 2008.
Background:	This unique Australian AD, issued in 1969, required modification to the tail rotor pedal control in accordance with Bell Service Bulletin 206A-5 to balance tail rotor pedal forces at cruise flight.  The AD compliance was before 1 September 1971.  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