As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED SLAT PANEL NR 2 INBD FACE XOS 238 RT WING. THE SLAT PANEL WAS REMOVED IAW AMM 27-80-01 000-806, HFEC INSPECTION WAS ACCOMPLISHED AND ONE CRACK WAS FOUND IAW NDT SPM 06-10-01. THE SLAT PANEL WAS REPAIRED IAW SRM 57-00-00 FIG. 201 AND INSTALLED IAW AMM 27-80-01 400-805 STEP E5 AND F.