Commonwealth legislation

AD/PA-32/64 - Fuel Flow Indicator Line - Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires owners/operators of specified Piper PA‑32RT‑300T serial numbers to replace the fuel‑flow indicator line per Piper Service Bulletin No. 652 or FAA AD 79‑13‑04 within 25 hours’ time‑in‑service after 19 July 1979. It’s mandatory maintenance aimed at preventing reported fuel leaks and engine power loss; operators pay for and must schedule the urgent work, with compliance dependent on access to the referenced documents and parts.

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Current sections

Direct links to the current provisions in AD/PA-32/64 - Fuel Flow Indicator Line - Replacement.

AD/PA-32/64 - Fuel Flow Indicator Line - 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-32 (Cherokee Six) Series Aeroplanes

AD/PA-32/64 Fuel Flow Indicator Line - Replacement 9/79

Applicability: Model PA-32RT-300T with S/Nos. 32R-7887001 to 32R-7987124. Document: 1. Piper SB No. 652; or

FAA AD 79-13-04, Amendment 39-3500.

Compliance: Within 25 hours time in service after 19 July 1979.

Background: There are overseas reports of broken fuel flow indicator lines which have resulted in fuel leakage, engine power loss and one instance of a forced landing.

Source text

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