AD/PA-34/5 - Stabilator Tip Balance Weight - Inspection

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

Legislation au F2006B05920 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-34/5 Stabilator Tip Balance Weight - Inspection 9/72

Applicability: All models with S/Nos. 34-E4 and 34-7250001 to 34-7250335. Document:  Piper SB No. 367.

Compliance: 1. Initial Inspection - prior to further flight after 12 September 1972.

 

2. Hardware Replacement - as detailed in requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.