Document ID: chunk:federal_register_of_legislation:F2006B07181:body:0
Version: federal_register_of_legislation:F2006B07181
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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/SWSA226/41 Flight Control, Control Column - Modification 2/82

            Applicability: All model SA226-T S/N T201 to T290. All model SA226-AT S/N AT001 to AT066 and all model SA226-TC S/N TC201 to TC225.

 Document: Swearingen SB27-022.

            Note: FAA AD 81-26-04 Amendment 39-4284 refers.

 Compliance: Within 300 hours time in service after 28 February, 1982.

            Background: There has been a failure of the control column cable pulley system with subsequent loss of lateral control reported overseas.