AD/BEECH 23/38 - Control Column Bearing Assemblies

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

Legislation au F2006B03752 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 19, 23 and 24 Series Aeroplanes

 

AD/BEECH 23/38 Control Column Bearing Assemblies 5/79

Applicability: All model B19 with S/Nos. MB-866 to MB-904.

 

All model C23 with S/Nos. M-1971, M-1980 to M-2076. All model C24R with S/Nos. MC-533, MC-537 to MC-611.

Requirement: Action in accordance with Beechcraft SI No. 1017. Compliance:  Within 100 hours time in service after 31 May 1979.

Background:  The manufacturer advises that the subject control column bearing assemblies may have been filed or ground in the weld area.

 

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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.