As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN L/H AT FR68 FLOOR AT L2 DOOR, HAS CORROSION AT 4EA FASTENER HOLES, MARKED IN RED GROUNDED - YES. REMOVED CORROSION AND REPAIRED DAMAGE AREA AT FR68 L/H SIDE ON L2 DOOR SILL IAW ASA A320 SRM 53-41-14-300--001 ORIGINAL MATERIAL THICKNESS IS .063 AT NUTPLATE HOLES REMOVED .031 REMAINING THICKNESS OF .032 ONLY ALLOWED 25% LOSS CATEGORY A