As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 6 SLAT HAS CORROSION IN SEAM BETWEEN NOSE UPPER SKIN ASSY AND LOWER AFT EDGE SKIN. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02 FIG 101, DET II. REMOVED COVE ANGLE IAW 51-40-02 INSTALLED COVE ANGLE & REPAIR SPLICE IAW SRM 51-40-02 & SRM 51-70-11 FROM OSS 106.0 - OSS 272.62 ON SLAT NR 6. MAJOR REPAIR.