Document ID: chunk:federal_register_of_legislation:F2006B03439:body:0:p2
Version: federal_register_of_legislation:F2006B03439
Segment Type: other
Provision Reference: 
Character Range: 2902–4056

inspections in an expanded area are now required.

            Amendment 1 required inspections to detect cracking and corrosion of the aft trunnion of the outer cylinder of the main landing gear, and various follow-on actions. It also provided for termination of the inspections by repairing the outer cylinder and installing new aft trunnion bushes.

            Amendment 2 clarified an inspection requirement of FAA AD 96-03-02 R1. Amendment 3 required implementation of the previously optional terminating action.
            Amendment 4 is issued in response to a new FAA AD which prohibits the use of a particular corrosion inhibiting compound during accomplishment of the terminating action.

            Amendment 3 of this Airworthiness Directive became effective on 30 January 1997. Amendment 2 of this Airworthiness Directive became effective on 20 June 1996.
            The original issue of this Airworthiness Directive became effective on 30 September 1995.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 8 March 2002

 The above AD is notified in the Commonwealth of Australia Gazette on 27 March 2002.