Document ID: chunk:federal_register_of_legislation:F2006B04208:body:0
Version: federal_register_of_legislation:F2006B04208
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 90 and 65-90 (King Air) Series Aeroplanes

AD/BEECH 90/14 Elevator Tab Hinge Beam - Inspection 7/68

 Applicability: All models in excess of 1000 hours total time in service.

            Requirement: Inspect the upper and lower flanges of the LH and RH elevator tab hinge beam P/N 50-610000-94 for cracking along the rivet line.

 Compliance: Forthwith and thereafter at intervals not exceeding 200 hours' time in service.