AD/BEECH 56/1 Amdt 2 - Rudder Spar and Hinges

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

Legislation au F2006B04041 Not 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 56TC (Turbo Baron) Series Aeroplanes

 

AD/BEECH 56/1

Amdt 2


Rudder Spar and Hinges 5/68

 

Applicability: Model 56TC with S/Nos. TG-1 to TG-51.

 

Requirement: Action in accordance with Beechcraft SB 67-34, Rev. 1.

 

Compliance: Inspect for cracking within 100 hours’ time in service from 16 May 1968 and thereafter at intervals not exceeding 100 hours’ time in service until modified. Modify and inspect for alignment within 300 hours’ time in service from 16 May 1968.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.