As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE / SKIN / FS 481-520 / STRG. 26L-26R : CORROSION REPAIR THE FUSELAGE SKIN WAS CORRODED IN SEVERAL AREAS BETWEEN FS 481 & 520 AND BETWEEN STRINGERS 26L & 26R. THE SKIN WAS CUT AT FS 520 BETWEEN THE LAP JOINT STRINGERS 26L & 26R. THE CORRODED SECTION OF SKIN WAS REMOVED AND REPLACED WITH A NEW SKIN. THE SKIN WAS SPLICED AT FS 520 WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 382204-14AD, REV A.