Commonwealth legislation

AD/BEECH 65/1 - Rudder Torque Tube Lowering Fitting - Inspection

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

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What this does This directive mandates a recurring safety inspection for a specific component in the rudder control system (the torque tube lowering fitting) on certain Beechcraft aircraft.

Who it affects Owners and operators of Beechcraft Model 65-80 Queen Air aeroplanes with serial numbers prior to LD-139.

What must be done The rudder torque tube lowering fitting must be inspected at intervals of no more than 100 hours of flight time, starting from 2 April 1964. The technical details of the inspection are found in Beechcraft Service Letter No. 64-6.

Why it matters This prevents potential mechanical failure in the rudder system, ensuring the pilot can maintain control of the aircraft's direction and stability during flight.

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Direct links to the current provisions in AD/BEECH 65/1 - Rudder Torque Tube Lowering Fitting - Inspection.

AD/BEECH 65/1 - Rudder Torque Tube Lowering Fitting - Inspection

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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 65 and 70 (Queen Air) Series Aeroplanes

AD/BEECH 65/1 Rudder Torque Tube Lowering Fitting - Inspection

Applicability: Model 65-80 with S/Nos. prior to LD-139. Document: Beechcraft SL No. 64-6.

Compliance: At intervals not exceeding 100 hours’ time in service after 2 April 1964.

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Source text

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