As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MCN - DURING C6 CHECK DISCOVERED LEVEL 2 CORROSION ON L2 DOOR THRESHOLD AT 2 FASTENER HOLES AT FRAME 68, WL Z-240 AND Y1295. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-14 FIG 101. DAMAGED AREA WAS CUT OUT IAW AIRBUS 320 SRM 53-41-14 FIG 201. FORMED REPAIR ANGLE AND FILLERS IAW AIRBUS 320 SRM 53-41-14 FIG 201. INSTALLED REPAIR PARTS AT FRAME 68, WL Z-240 AND Y1295 AT THE L2 DOOR THRESHOLD IAW AIRBUS 320 SRM 53-41-14 FIG 201.