Commonwealth legislation

AD/BEECH 56/21 - Control Surface Trim Tab Systems

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires owners/operators of Beechcraft 56TC and A56TC Turbo Baron aircraft (serials TG-2 through TG-94) to inspect the control surface trim tab systems per Beechcraft Service Instruction No. 0846-152, Revision 2. Inspections start within 100 flight hours after 30 June 1980 and repeat every 100 hours to detect wear/free play that could degrade control and ensure continued flight safety.

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Current sections

Direct links to the current provisions in AD/BEECH 56/21 - Control Surface Trim Tab Systems.

AD/BEECH 56/21 - Control Surface Trim Tab Systems

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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 56TC (Turbo Baron) Series Aeroplanes

AD/BEECH 56/21 Control Surface Trim Tab Systems 6/80

Applicability: All models 56TC and A56TC with S/Nos. TG-2 to TG-94. Requirement: Action in accordance with Beechcraft SI No. 0846-152, Rev. 2.

Compliance: Within 100 hours’ time in service after 30 June 1980 and thereafter at intervals not exceeding 100 hours’ time in service.

Background: The inspection procedure defines maximum allowable control surface trim tab free play caused by accumulative wear in control linkage and actuators.

Source text

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