AD/SWSA226/6 - Trim Tab Actuator Rods - Inspection
1AD/SWSA226/6 - Trim Tab Actuator Rods - Inspection
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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 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.