AD/PA-32/38 - Quick Disconnect Seat Retention Mechanism - Inspection

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Legislation au F2006B05833 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-32 (Cherokee Six) Series Aeroplanes

 

AD/PA-32/38 Quick Disconnect Seat Retention Mechanism - Inspection


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Applicability: Model PA32-260 with S/Nos. 32-01 to 32-7500002. Model PA-32-300 with S/Nos.

32-40001 to 32-7540028.

 

Document: Piper SL No. 763.

 

Compliance: Within 100 hours time in service after 30 January 1976.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.