AD/AC/39 - Wing Front Spar Lower Cap - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B02097 Not 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

 


Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

 

AD/AC/39 Wing Front Spar Lower Cap - Inspection 2/68

Applicability: All 560E, 680 and 680E models.

 

Requirement:  Inspect the wing front spar lower cap between wing stations 67 and 86, left and right hand sides, using radiographic technical DCA NDI/R/1 or other technique approved by the Secretary, for damaged or double drilled holes, poor rivet fit or cracking.

 

Compliance: Within 100 hours time in service after 22 February 1968.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.