As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 736. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D.028. ORIG MATERIAL .063 AFTER REWORK .035 FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5750-146287. MAJOR REPAIR