Document ID: chunk:federal_register_of_legislation:F2006B03722:body:0
Version: federal_register_of_legislation:F2006B03722
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/7 Rudder Push Rod Assembly 5/76

 Applicability: All models with S/Nos BB-2 to BB-58.

 Requirement: Action in accordance with Beechcraft SI No 0778-153.

            Note: FAA AD 76-03-07 refers.

 Compliance: Within 100 hours time in service after 31 May 1976.