AD/Bell 212/33 Main Rotor Grip/Blade Bolt Inspection and Rework 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 212/33.

Bell Helicopter Textron 212 Series Helicopters

AD/BELL 212/33 Main Rotor Grip/Blade
Bolt - Inspection and Rework 4/2009

Requirement:	CANCELLED.
This AD is cancelled on 9 April 2009.
Background:	This unique Australian AD, issued in 1985, required a one off inspection of the main rotor grip blade and bolt for blade/bolt interference in accordance with Bell ASB Bell SB No. 212-85-37.  The AD compliance was within 100 hours time in service or at the next scheduled inspection after 31 March 1985.  As all aircraft would have been inspected by now, the AD is no longer required.

David Punshon
Delegate of the Civil Aviation Safety Authority

3 February 2009