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

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Legislation au F2006B07567 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.