Commonwealth legislation

AD/PA-24/26 Amdt 1 - Pitch Trim Switch - Modification

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive mandates modification of the pilot’s rocker-type pitch trim switch on Piper PA-24-260 aircraft with serial numbers 24-4783 to 24-5047, to be done per Piper Service Bulletin No. 527 or FAA AD 77-09-10 within 100 hours TIS after 28 Feb 1977.

It affects owners/operators, who must fund and arrange the specified modification to maintain airworthiness; it matters because compliance is mandatory and limits remediation to the two prescribed technical procedures.

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AD/PA-24/26 Amdt 1 - Pitch Trim Switch - Modification

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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-24 (Comanche) Series Aeroplanes

AD/PA-24/26

Amdt 1

Pitch Trim Switch - Modification 5/71

Applicability: Model PA-24-260 with S/Nos. 24-4783 to 24-5047 fitted with rocker type trim switch on pilot’s control wheel.

Document: 1. Piper SB No. 527; or

FAA AD 77-09-10.

Compliance: Within 100 hours time in service after 28 February, 1977.

Source text

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