AD/PC-6/28 Amdt 1 - Wing Strut Attachment - Inspection

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

Legislation au F2006B06131 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-6/28

Amdt 1


Wing Strut Attachment - Inspection 12/80

 

Applicability: All models with S/Nos. 338 to 701. Document:  Pilatus SB No. 93.

Compliance: At intervals not exceeding 100 hours time in service.

 

Background:  Service experience indicates that the inspection for corrosion in the wing strut attachment can be extended to 100 hourly intervals.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.