AD/PA-23/72 - Auto Pilot Servo Bridle Clamp Bolt Torque - Modification

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

Legislation au F2006B05499 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-23/72 Auto Pilot Servo Bridle Clamp Bolt Torque - Modification

Applicability: Model PA23-250 with S/Nos. 27-4575 to 27-7754077. Document:  Piper SB No. 558.

Compliance: Within 100 hours time in service after 30 September 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.