As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 10 SLAT HAS CORROSION IS SEAM BETWEEN UPPER NOSE WEDGE SKIN & AFT EDGE SKIN ASSY. REMOVED CORROSION ON NR 10 SLAT COVE ANGLE IAW SRM 51-10-02 BLEND OUT DIM L 131" ,W 1.0", D.20". FOUND OUT OF LIMITS IAW SRM 57-43-02 FIG 10, DET 2 COMPLIED WITH EA NR F-5740-131183 ON NR10 SLAT COVE ANGLE SPLICE REPAIR OSS 736.70 - 768.0, PN 114N4002-8. THIS IS A MAJOR REPAIR.