As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND CORROSION AND DISHED RIVETS IN LT FUSELAGE SKIN JUST FORWARD OF NR 2 ENGINE FORWARD COWL, STA 1352, S20L. THE FASTENERS WERE REMOVED IAW SRM 53-30-3. THE CORRODED SKIN WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.