As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 10 SLAT COVE ANGLE CORRODED. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. ORIG MATERIAL .063 AFTER REWORK .000 MATERIAL LOSS .063 FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101, DETAIL II. L= 131" X W=2" X D=.063. R & R COVE ANGLE IAW SRM 51-40-02. CLASSIFIED MAJOR REPAIR.