As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL PANEL ON WING LEADING EDGE BETWEEN NR 9 SLAT INBOARD AND OUTBOARD AUX TRACKS CORRODED AROUND NUTPLATE AT LES .595. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NOSE BEAM IAW DWG 114T2300. INSTALLED IAW SRM 51-40-02, PARA 4.7.10.