AD/PA-23/74 - Stabilator Trim Control Rod to Tab Attachment - Inspection

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

Legislation au F2006B05501 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-23 (Apache and Aztec) Series Aeroplanes

 

AD/PA-23/74 Stabilator Trim Control Rod to Tab Attachment - Inspection


4/78

 

Applicability: All model PA23-250(6) place Aztec “F” with S/Nos. 27-7754118, 27-7754129,

27-7754130, 27-7754132, 27-7754137, 27-7754145 to 27-7754152, 27-7754154 to

27-7754156, 27-7754158 to 27-7854007, 27-7854009 to 27-7854813, 27-7854015

to 27-7854017, 27-7854019 to 27-7854023, 27-7854025 to 27-7854029,

27-7854031 to 27-7854033, 27-7854035, 27-7854037 and 27-7854038.

 

Document: Piper SB No. 590.

 

Compliance: Within 100 hours time in service after 30 April 1978.

 

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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.