As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND LEFT CENTER FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 720A, STRINGER 26L. THE CORRODED AREA WAS CUT OUT AND THE CORROSION WAS CLEANED IAW SRM 51-10-6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-30-3, AND 51-30-2.