AD/VAT/20 - Centre Flap Spar - Inspection

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Legislation au F2006B07553 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/20 Centre Flap Spar - Inspection 6/64

Applicability: Victa Airtourer 100 and 115 not incorporating Victa Mod. B141 and which have exceeded 500 hours time in service.

 

Requirement: Inspect the centre flap spar in the region of the actuating bracket P/N 16105/1 for cracking. If cracking is found repair in accordance with an approved scheme before further flight.

 

Compliance: At intervals not exceeding 100 hours time in service, after 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.