AD/BEECH 23/42 - Engine Control Rod Safety Washers

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

Legislation au F2006B03756 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 23/42 Engine Control Rod Safety Washers 8/83

Applicability: Models A23-19, 19A, M19A and B19 with S/Nos. MB-1 to MB-520. Model B19 Sport 150 with S/Nos. MB-521 to MB-905.

 

Models 23, A23, A23A, B23 and C23 with S/Nos. M-2 to M-1361. Model C23 Sundowner 180 with S/Nos. M-1362 to M-2348.

Models A23-24 and A24 with S/Nos. MA-1 to MA-368. Model A24R with S/Nos. MC-2 to MC-95.

Models A24R, B24R and C24R Sierra 200 with S/Nos. MC-96 to MC-769.

 

Requirement: Action in accordance with Beechcraft SI No. 1243. Compliance:  Within 100 hours time in service after 30 September 1983.

Background:  The manufacturer considers it necessary to install a safety feature to the engine control rod ends.

 

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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.