Commonwealth legislation

AD/PA-30/13 Amdt 1 - Pitch Trim Switch - Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The directive mandates replacing a rocker‑type pitch‑trim switch on the pilot’s control wheel of specified Piper PA‑30 and PA‑39 aeroplanes (listed by serial number), using the procedures in Piper Service Bulletin No. 527 or FAA AD 77‑09‑10, within 100 hours TIS after 28 Feb 1977. Owners/operators of affected aircraft bear the cost; aircraft already compliant under earlier issues are treated as compliant.

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AD/PA-30/13 Amdt 1 - Pitch Trim Switch - Replacement

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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-30 & 39 (Twin Comanche) Series Aeroplanes

AD/PA-30/13

Amdt 1

Pitch Trim Switch - Replacement 2/77

Applicability: Model PA-30 with S/Nos. 30-1717 and 30-1745 to 30-2000 and all model PA-39 with S/Nos. 39-1 to 39-155 fitted with rocker type 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.

Note: Aircraft complying with previous issues of this Directive, satisfy this issue of the Directive.

Source text

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