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

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

Legislation au F2006B04208 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 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.