WPR10CA314
WPR10CA314

The pilot reported that during an aerial application flight the engine lost power due to fuel exhaustion. The pilot reported that there were no mechanical abnormalities with the engine or airframe. The helicopter’s fuel system was not inspected by the NTSB or the FAA because the helicopter was in the process of being disassembled prior to the NTSB or FAA being notified of the accident.

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