Document ID: chunk:federal_register_of_legislation:F2006B10619:body:0:p2
Version: federal_register_of_legislation:F2006B10619
Segment Type: other
Provision Reference: 
Character Range: 2896–3990

2004, whichever occurs first.

           The compliance times for Requirement 1 remain unchanged by this issue. This Amendment becomes effective on 10 June 2004.

           Background: A fatal accident report indicated that the cause was fatigue failure of a centre frame aft cluster fitting.

           Amendment 2 clarified that all aft cluster fittings have to be dye-penetrant inspected.

           Amendment 3 aligned this Directive with the requirements of the related FAA AD for part number 269A2234 and 269A2235 aft cluster fittings, and introduced optional terminating action for the repetitive inspection requirements of this Directive.

           Amendment 4 is issued in response to the related FAA AD, which requires unmodified basic part number aft cluster fittings to be removed from service.

           Amendment 2 of this Airworthiness Directive became effective on 3 March 1995.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 29 April 2004

 The above AD is notified in the Commonwealth of Australia Gazette on 19 May 2004.