Document ID: chunk:federal_register_of_legislation:F2006B02538:body:0:p2
Version: federal_register_of_legislation:F2006B02538
Segment Type: other
Provision Reference: 
Character Range: 3755–5167

that the lives are listed in the Maintenance Manual; however they are in fact listed in the Owners Manual.

            This Amendment becomes effective on 27 June 2001.

            Background: Airframe component life limitations determined by the manufacturer have been published in the Airworthiness Limitations section of the Owners Manual.
            Amendment 1 included new and revised lives for some landing gear components. Amendment 2 implemented extended lives for wing and fin spar components and expressed tail gear spring lives in landings as well as hours, as for the MLG spring leg lives. This Amendment follows further information received from the manufacturer, and clarifies aircraft serial number applicability for the fin component lives. A part number error has also been corrected.

            Amendment 4 is issued to delete the wing spar cap retirement lives from the retirement schedule; as the retirement lives are now contained in AD/AT 800/3.

            Amendment 3 of this Airworthiness Directive became effective on 10 August 2000. Amendment 2 of this Airworthiness Directive became effective on 13 July 2000.
            The original issue of this Directive became applicable on 15 August 1996.

 David Alan Villiers
 Delegate of the Civil Aviation Safety Authority 21 June 2001

 The above AD is notified in the Commonwealth of Australia Gazette on 27 June 2001.