AD/PA-34/22 - Fuselage Structure Rivets - Inspection

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

Legislation au F2006B05893 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-34 (Seneca) Series Aeroplanes

 

AD/PA-34/22 Fuselage Structure Rivets - Inspection 3/77

Applicability: All model PA-34-200 with S/Nos. 34-7250001 to 34-7450220. All model PA-34-200T with S/Nos. 34-7570001 to 34-7670292.

Document: Piper SB No. 545.

 

Compliance: Within 100 hours time in service after 31 May 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.