Commonwealth legislation

AD/PA-32/60 - Manually Trippable Breaker for Pitch Trim Circuit - Installation

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

1/10 complexity

Owners of specific Piper PA‑32 Cherokee Six models (listed serial ranges) fitted with an Altimatic IIIC autopilot must install a manually trippable circuit breaker in the pitch‑trim circuit per Piper Service Bulletin No. 622. This lets pilots immediately kill trim power to stop potential autopilot‑induced runaway trim, improving safety. Compliance: within 100 flight hours after Jan 31, 1979.

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AD/PA-32/60 - Manually Trippable Breaker for Pitch Trim Circuit - Installation

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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 Piper PA-32 (Cherokee Six) Series Aeroplanes

AD/PA-32/60 Manually Trippable Breaker for Pitch Trim Circuit - Installation

3/79

Applicability: Model PA-32-260 with S/Nos. 32-7500001 to 32-7700023; Model PA-32-300 with S/Nos. 32-7540001 to 32-7840083; Model PA-32R-300 with S/Nos. 32R-7680001 to

32R-7880066 fitted with Altimatic IIIC automatic pilot.

Document: Piper SB No. 622.

Compliance: Within 100 hours time in service after 31 January 1979.

Source text

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