Commonwealth legislation

AD/PA-44/5 - Engine Priming System - Modification

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Piper PA-44-180 serials 44-7995001 through 44-7995190 to have the engine fuel priming system modified within 25 hours TIS after 29 June 1979, following Piper SB No. 634 or FAA AD 79-12-11. It responds to reported cracking and fitting failures that create a fire hazard; compliance and associated costs and scheduling fall to the affected aircraft owners/operators.

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AD/PA-44/5 - Engine Priming System - 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-44 (Seminole) Series Aeroplanes

AD/PA-44/5 Engine Priming System - Modification 8/79

Applicability: Model PA-44-180 with S/Nos. 44-7995001 to 44-7995190. Document: 1. Piper SB No. 634; or

FAA AD 79-12-11, Amendment 39-3490.

Compliance: Within 25 hours time in service after 29 June 1979.

Background: The engine fuel primer system of this aircraft is subject to cracking of lines and breakage of fittings and poses a fire hazard.

Source text

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