AD/PA-22/18 - Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation
1AD/PA-22/18 - Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.