As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND EXTERNAL FUSELAGE SKIN LAP BULGED AND ONE FASTENER SHEARED AT FS 380, STRINGER 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2, 53-30-2 AND 51-30-2.