Document ID: chunk:federal_register_of_legislation:F2006B03939:body:0
Version: federal_register_of_legislation:F2006B03939
Segment Type: other
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Beechcraft 50 (Twin Bonanza) Series Aeroplanes

AD/BEECH 50/15 Elevator Trim Tab Hinge Beam 12/65

 Applicability: All models.

            Requirement: Visually inspect the elevator trim tab hinge beam (P/N 50/610000/94) for cracking in the flange and web.

 Compliance: At intervals not exceeding 250 hours' time in service.