As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE INSPECTING RT OUTER WING SPAR AS PER TASK 5710/08A, CHAFING DAMAGE WAS NOTED ON THE R/H WING FLUX VALVE WIRING HARNESS WHERE IT PASSES THROUGH THE ORCON TAPE COVERING THE FORWARD SPAR LIGHTENING HOLES. DAMAGE LOCATION AT YW 502.50.