AD/PA-32/11 - Wing Rear Spar Attach Bolts - Inspection

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

Legislation au F2006B05805 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Piper PA-32 (Cherokee Six) Series Aeroplanes

 

AD/PA-32/11 Wing Rear Spar Attach Bolts - Inspection 1/68

Applicability: As detailed in Piper SB No. 261. Document:  SB No. 261.

Compliance: Within 100 hours time in service after 25 January 1968.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.