As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS FOUND WITH CORROSION AT FS 1610 BETWEEN STRINGERS 28L & 29R. THE UNDERLYING STRINGERS ALSO HAD AREAS OF CORROSION. THE STRINGERS WERE REPAIRED WITH CHANNEL SECTIONS PER THE SRM. THE SKIN DAMAGE WAS REMOVED WITH A 10 X 4 INCH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384582-14, REV A.