As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, INTERNAL FUSELAGE AT BS 882-RT FOUND CORROSION ON FWD SIDE OF WINDOW BELT/SHIN DOUBLER BETWEEN STR 20 AND 22. CORROSION REMOVED ACC SRM 51-10-01, OUT OF LIMITS. ACCORDING TO EFN 747-53-1168, MAX BLEND OUT .055 INCH. SHIN PANEL REPAIRED ACCORDING EFN 747-53-1192.