AD/PA-22/18 - Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation

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

Legislation au F2006B05422 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-22 (Tri-Pacer and Colt) Series Aeroplanes

 

AD/PA-22/18  Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation


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Applicability: All models.

 

Requirement: Modify the horizontal stabiliser trim control screw mechanism by installing a stop to prevent the yoke assembly (P/N 42692-00) from binding against the pulley (P/N 12982-00) when the mechanism is wound to the extreme nose-down position.

 

Note: W.E. James Aircraft Pty. Ltd. Drawing No. WEJ-65 covers an approved means of compliance.

 

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.