As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING NR1 SLAT ERODED ABOVE NR1 PYLON, BLEND OUT THE EROSION AREA TO SMOOTH CONTOUR AND MEASURED THE AREA MAX DIMENSION IS 4" * 0.9" AND (3) LAYERS DAMAGED, THEN REPAIRED WITH FIBERGLASS AND RESIN COMPOUND. (CURE AT 180 DEGREE F) IAW EA NR 6-5750-141608. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.