AD/Bell 205/42 Main Rotor Hub Inboard Fitting Life Reduction 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 205/42.

Bell Helicopter Textron 205 Series Helicopters

AD/BELL 205/42 Main Rotor Hub Inboard
Fitting - Life Reduction 3/2009

Requirement:	CANCELLED.
This AD is cancelled on 12 March 2009.
Background:	This unique Australian AD, issued in 1978, required retirement of the main rotor hub inboard fitting in accordance with Bell ASB Bell SB No. 205-78-3.  As this requirement is now contained in the mandatory airworthiness limitations schedule of the maintenance manual, the AD is no longer required.

David Punshon
Delegate of the Civil Aviation Safety Authority

28 January 2009