As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING NR 8 SLAT CORRODED AT THE TIA ATTACH POINT TO SLAT. BLENDED CORROSION ON CHORD SPLICE ANGLE ON NR 8 SLAT AT TAI ATTACH POINT. REMOVED .020 FROM NOMUAL .100 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-43-02 FIG 101 DETAIL V. REMOVED AND REPLACED ANGLE, IAW B767 SRM 51-40-02 PARA 7.