As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUEL PUMP WIRING HARNESS IS NOT SUPPORTED WITHIN THE FUEL CELL AND CHAFED ON THE FUEL LINE FROM THE PRIMARY PUMP TO THE CHECK VALVE INSIDE THE FUEL CELL. THERE WAS .006 INCH DAMAGE TO THE WALL OF THE FUEL LINE AND THE PUMP HARNESS SHIELDING WAS CHAFED THROUGH. THERE WAS NO EVIDENCE OF ARCING.