Document ID: chunk:federal_register_of_legislation:F2006B09650:body:0:p2
Version: federal_register_of_legislation:F2006B09650
Segment Type: other
Provision Reference: 
Character Range: 2983–4045

the accomplishment of an etch penetrant inspection to terminate the necessity for further repetitive eddy-current inspections, and rework or replacement of any fitting when cracks are found. Recent tests and analysis have shown that a limited number of repeat inspections, combined with a final etch penetrant inspection during overhaul (or "on aircraft") is sufficient to restore the safe life condition of the Main Landing Gear Main Fitting.

            Amendment 4 is issued to correct the Requirement 2.a. document number. Amendment 3 of this Airworthiness Directive became effective on 2 October 2003. Amendment 2 of this Airworthiness Directive became effective on 18 April 2002.
            Amendment 1 of this Airworthiness Directive became effective on 27 December 2001.

            The original issue of this Airworthiness Directive became effective on 29 November 2001.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 16 September 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 8 October 2003.