AD/PC-6/38 - Horizontal Stabiliser Inspection

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

Legislation au F2006B06142 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-6/38 Horizontal Stabiliser Inspection 7/93

Applicability: All Pilatus Porter PC-6 series aircraft. Requirement:  Retire the horizontal stabiliser; or

Modify the horizontal stabiliser and inspect for cracks in accordance with a scheme approved by the Authority.

Note: Aeronautical Designs Australia Pty Ltd EO-934 is an approved scheme for the purpose of this Directive.

Compliance: Retire before 10000 hours component time in service; or

 

Modify and inspect before 10000 hours component time in service. Re-inspect at intervals not exceeding 100 hours.

Background: The Pilatus Porter horizontal stabiliser has a history of fatigue cracking in service.

Inspection access to some cracking sites is very restricted.

 

This AD gives two options: retire before cracks are likely to start; or improve access and inspect.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.