Rowesville, SC, USA
N7355W
PIPER PA 28
Same as Factual Information
The pilot reported that about 20 minutes after takeoff the engine experienced a total loss of power. The pilot further reported that during the off airport forced landing the right aileron was substantially damaged. A post-accident examination revealed that the fuel line between the fuel transducer and the carburetor had failed. The manufacture and part number for the failed line was Strato Flex, P/N 111-6, respectively. The fuel line was installed as part of the J. P. Instruments EDM-700 engine monitoring system per the supplemental type certificate SA2586NM on May 01, 2002.
The fuel line failure between the fuel transducer and the carburetor, which resulted in a total loss of engine power and subsequent forced off airport landing.
Source: NTSB Aviation Accident Database
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