Commonwealth legislation

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

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Commonwealth Airworthiness Directive mandates that owners/operators of the specified Beechcraft aeroplanes (listed by model and serial number) must carry out the action in Beechcraft Service Instruction No. 0994 concerning the stabilator trim tab actuator rod.

The work must be completed within 25 hours time in service after 3 July 1978; affected owners/operators bear the cost and scheduling burden to comply.

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

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.