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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B05861 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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

2. 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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.