NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.
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.