As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SPEC. NO. JE17-5341-1-2710, L2 DOOR SILL PLATE AT FR68L CORRODED AFT OF GIRT BAR PLATE, REMOVED CORROSION ORIGINAL THICKNESS 0.03 MATERIAL LOSS .0.037 M AX MATERIAL LOSS 0.0157 FOUND TO BE OUT OF LIMITS IAW A319 SRM 5 3-41-14-283-002 FIG. 10101. REPAIRED L-2 DOOR SILL PLATE AT FR68 L IAW A319 SRM 53-41-14-300-001 REPAIR PRINCIPLE 7.