As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLOOR SUPPORT AT FS 349.00 LT SIDE UNDER PANEL 231CLF CORRODED. CLEAN CORROSION IAW 51-21-06 AND VERIFY LIMITS. REMOVED CORROSION FROM FS 349 CROSSBEAM AT LBL 40, WL 73, TOP FLANGE IAW SRM 51-21-06. REPAIR DIMENSIONS: 1"X 1.5" X .003" DEEP ORIGINAL THICKNESS .063", REMAINING THICKNESS .060" WITHIN ALLOWABLE LIMITS OF SRM 53-00-00, FIG 102.