As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 665.5. REMOVED CORROSION FROM COVE PNL IAW SRM 51-10-02. BLEND OUTDIM=3.0" LX 1,0"W X .010" D, ORIGINAL MAT'L. THICK .050, MAT'L AFTER REWORK .04" FOUND OUT OF LIMITS IAW. SRM 57-43-01 FIG. 101 DET. VI. FABRICATED COVE PNL ON MAE TRAVELER NR T10/837840. MINOR REPAIR.