AD/PC-6/31 - Wing Strut Internal Corrosion - Inspection

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

Legislation au F2006B06135 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pilatus Porter PC-6 Series Aeroplanes

 

 

AD/PC-6/31

Wing Strut Internal Corrosion - Inspection

7/71

Applicability:

All models except Fairchild Hiller production.

 

Document:

Pilatus SB No. 105.

 

 

Compliance: Within 100 hours time in service after 31 August 1971 and thereafter at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.