Document ID: chunk:federal_register_of_legislation:F2006B03692:body:0:p2
Version: federal_register_of_legislation:F2006B03692
Segment Type: other
Provision Reference: 
Character Range: 2920–3683

fitting lug holes, reducing their susceptibility to fatigue failure.

           Amendment 5 makes a correction to the applicability of Requirement 2.

           Amendment 6 incorporates revised wing spar shear attachment fitting fatigue lives of 30000 hours time in service with an associated inspection schedule. These extensions to the aircraft fatigue lives have been accepted by CASA for Australian operators, based on a critical review of the manufacturer's fatigue test results.
           Amendment 5 of this airworthiness directive became effective on 14 September 1995. Amendment 4 of this airworthiness directive became effective on 5 September 1991. The original issue of this airworthiness directive became effective on
           30 September 1981.