AD/PA-24/43 - Wing Main Spar Lower Cap - Inspection

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

Legislation au F2006B05542 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-24 (Comanche) Series Aeroplanes

 

AD/PA-24/43 Wing Main Spar Lower Cap - Inspection 9/83

Applicability: All model PA-24-400 with S/Nos. 26-2 and subsequent. All model PA-24-180, PA- 24-250 and PA-24-260 with S/Nos. 24-1 and subsequent.

 

Document: Piper Service Bulletin No. 751.

 

Compliance: Within 100 hours time in service after 30th September 1983.

 

Background: The manufacturer reports cases of chafing of the wing main spar lower cap where the spar enters the fuselage.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.