As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT LOWER SPAR CAP BEHIND INNER FENDER WAS CHAFED BY FUEL PRESSURE SWITCH LINE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED , ALODINED AND PRIMED THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.