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 574.80. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24" W= 1.0" D=.010". ORIG. MAT. .050 REMAINING .040 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET VII. FABRICATED COVE PANEL ON TRAVELER NR T10/837837. MINOR REPAIR