As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AVIONICS BAY FUSELAGE BEAM AT FS 349.00 BETWEEN S26L-R IS CORRODED ON THE FWD SIDE. REMOVE CORROSION & FASTENERS AS REQUIRED. EVALUATE 349 FRAME. REMOVED CORROSION IAW SRM 51-42-06 AND 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREA OF FRAME SECTOR IAW MAC NDT INSP PROCEDURE UT-3 MININMUM MATERIAL REMAINING IS .060". REPAIRED IAW REO 601R-53-21-1299.