As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-04 CHECK INTERGRANULAR CORROSION WAS FOUND ON R-2 DOOR SILL AT UPPER IB END BETWEEN FR 66 AND FR 68. MAINTENANCE CUTOUT DAMAGED AREAS OF R-2 DOOR SILL AT UPPER IB END, BOTH AT FR 68; FABRICATED A REPAIR DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW A320 SRM 53-41-14, FIG. 201.