AD/BEECH 50/15 - Elevator Trim Tab Hinge Beam

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03939 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.