AD/PA-34/33 - Window Curtain Rod Support Area - Inspection

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

Legislation au F2006B05905 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-34 (Seneca) Series Aeroplanes

 

AD/PA-34/33 Window Curtain Rod Support Area - Inspection 10/79

Applicability: All model PA-34-200T with S/Nos. referenced in Piper SB No. 656. Document:  Piper SB No. 656.

Compliance: Within 100 hours time in service after 30 November 1979.

 

Background: Damage to the fuselage longerons at the lower window line may have been caused when installing the window curtain rods at manufacture.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.