As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN PASSENGER CABIN CORROSION SEVERAL PLACES ON FLOOR PANEL NR 96 STA 1032. REMOVED CORROSION IAW SRM 51-10-3. ORIG THICKNESS WAS .025 AFTER BLEND MATERIAL IS .018. OUT OF LIMITS IAW SRM 53-01. FABRICATED NEW PANEL WEB AND HAT CHANNELS IAW DWG 9919601. INSTALLED HAT CHANNELS TO WEB IAW ERA 488335-14 P-134 09 JAN 11. REQUIRED INSP COMPLETED.