Document ID: chunk:federal_register_of_legislation:F2006B07567:body:0
Version: federal_register_of_legislation:F2006B07567
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Victa and A.E.S.L. Airtourer Series Aeroplanes

AD/VAT/33 Control Column Bearing Spigot Bolt - Inspection 10/68

 Applicability: Airtourer 100 and 115.

            Requirement: Inspect the control column torque tube near bearing spigot bolt P/N 31724/1 for conformity with 6/15-24 WNF-2A threadform.

            Note: The outside diameter of this thread should be 0.3042 inches minimum and the root diameter should be 0.2536 inches minimum.

            Compliance: Within 100 hours time in service after 6 October 1968 or before installation after 6 October 1968 whichever occurs first.