Commonwealth legislation

AD/BEECH 56/1 Amdt 2 - Rudder Spar and Hinges

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This Act has been repealed and is no longer in force. It is retained for historical reference.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 directive requires owners/operators of Beechcraft Model 56TC (Turbo Baron) serial TG-1 through TG-51 to inspect the rudder spar and hinges for cracking within 100 flight hours from 16 May 1968 and every 100 hours thereafter until a mandated modification is done. The modification and alignment check must be completed within 300 flight hours. The rule prevents in‑flight rudder failure; repair details are in Beechcraft Service Bulletin 67‑34, Revision 1.

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AD/BEECH 56/1 Amdt 2 - Rudder Spar and Hinges

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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 56/1

Amdt 2

Rudder Spar and Hinges 5/68

Applicability: Model 56TC with S/Nos. TG-1 to TG-51.

Requirement: Action in accordance with Beechcraft SB 67-34, Rev. 1.

Compliance: Inspect for cracking within 100 hours’ time in service from 16 May 1968 and thereafter at intervals not exceeding 100 hours’ time in service until modified. Modify and inspect for alignment within 300 hours’ time in service from 16 May 1968.

Source text

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