AD/PA-32/64 - Fuel Flow Indicator Line - Replacement
1AD/PA-32/64 - Fuel Flow Indicator Line - Replacement
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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
- 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.