AD/PA-25/29 - Wing Strut - Inspection

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

Legislation au F2006B05565 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

 


Piper PA-25 (Pawnee) Series Aeroplanes

 

AD/PA-25/29 Wing Strut - Inspection 4/69

Applicability: All models with lift struts which have exceeded 1500 hours total time in service.

 

Requirement: Inspect the lower ends of the wing lift struts for cracking particularly in the threaded area of the rear spar attachment using at least a 10X glass.

 

Compliance: Within 100 hour time in service after 15 April 1969 and thereafter at intervals not exceeding 500 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.