AD/SWSA226/6 - Trim Tab Actuator Rods - Inspection

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

Legislation au F2006B07201 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

 


Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 

AD/SWSA226/6 Trim Tab Actuator Rods - Inspection 8/72

Applicability: All models.

 

Requirement: Inspect for security of roll pin and for tightness of the rod in the socket of the end fitting on all trim tab actuator rods whose fixed ends are secured by roll pins.

 

Compliance: Within 25 hours time in service after 17 August 1972 and thereafter at intervals not exceeding 300 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.