AD/BEECH 23/36 - Stabilator Trim Tab Actuator Rod

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

Legislation au F2006B03750 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 23/36 Stabilator Trim Tab Actuator Rod 8/78

Applicability: Models B19 with S/Nos. MB-558 through MB-886.

 

Models C23 with S/Nos. M-1413, M-1414, M-1416 to M-1418, M-1420 to M-1422, M-1424 to M-1438, M-1440 to M-1446, M-1448 to M-2009, M-2011 to M-2015, M-2017 to M-2020.

 

Models B24R and C24R with S/Nos. MC-151 to MC-559, MC-561 to MC-563, MC-565 to MC-568, MC-571.

 

Requirement: Action in accordance with Beechcraft SI No. 0994. Compliance:  Within 25 hours time in service after 3 July 1978.

 

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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.