As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 8 SLAT T/E LWR SKIN CHAFED. REMOVED DAMAGED SKIN, REMOVED CORE, FABRICATED REPAIR PARTS AND BONDED IAW SRM 57-43-01, FIG 1 & 51-70-10, FIG 202 SHT NR 8 REPAIR NR4 R & R SLAT IAW MM 27-81-02. OPS CHECK ON NR 22, ZONE 520. PAINTED IAW MM 51-24-13. EXT. DOUBLER DIMS. 8.20" X 5.70 INTERNAL DOUBLER DIMS. 4.4" X 3.9" FILLER DIMS. 1.2" X 2.4".