Commonwealth legislation

AD/PA-30/1 - Fuel Valve Control Stop - 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This Act has been repealed and is no longer in force. It is retained for historical reference.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

This mandatory Airworthiness Directive requires owners/operators of Piper PA‑30 Twin Comanche aircraft (serial numbers below 30‑132, per Piper Service Letter No. 408) to install a fuel valve control stop. Compliance is immediate—must be done before flight—to prevent unsafe fuel‑valve movement that could cause engine fuel starvation.

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Current sections

Direct links to the current provisions in AD/PA-30/1 - Fuel Valve Control Stop - Installation.

AD/PA-30/1 - Fuel Valve Control Stop - 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-30 & 39 (Twin Comanche) Series Aeroplanes

AD/PA-30/1 Fuel Valve Control Stop - Installation 12/63

Applicability: Model PA-30 with S/Nos. below 30-132 as detailed in compliance document. Document: Piper SL No. 408.

Compliance: Forthwith.

Source text

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