Document ID: chunk:federal_register_of_legislation:F2006B05861:body:0
Version: federal_register_of_legislation:F2006B05861
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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.