Commonwealth legislation

AD/PA-28/54 - Spin Prohibition Placard

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of specified Piper PA-28-180s (S/N 28-7305001 to 28-7505079) to install a Spin Prohibition placard per Piper SB No. 436 within 25 hours TIS after 20 Jan 1975. It affects owners/operators and maintenance providers, imposes a small one‑off compliance cost and administrative task, and is enforced through the airworthiness directive mechanism (Civil Aviation Safety Authority).

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Current sections

Direct links to the current provisions in AD/PA-28/54 - Spin Prohibition Placard.

AD/PA-28/54 - Spin Prohibition Placard

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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-28 Series Aeroplanes

AD/PA-28/54 Spin Prohibition Placard 2/75

Applicability: Model PA28-180 with S/Nos. 28-7305001 to 28-7505079. Document: Piper SB No. 436.

Compliance: Within 25 hours time in service after 20 January 1975.

Source text

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