As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN PASSENGER CABIN CORROSION ON FLOOR PANEL PN37, SEVERAL PLACES. REMOVED CORROSION IAW SRM 51-10-3. ORIGINAL THICKNESS WAS .025 AFTER MATERIAL IS .005. OUT OF LIMITS IAW SRM 53-01. FABRICATED FLOOR PANEL WEB FROM 7075-T6 .025 AND HAT CHANNELS FROM S2912282T, PO 1022506 IAW ER/A 488330-14. ASSEMBLED FLOOR PANEL WEB AND HAT CHANNELS IAW ER/A 488330-14. REQUIRED INSP COMPLETED.