As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-07 CHECK A .5 INCH CRACK WAS FOUND ON LT WING LEADING EDGE SKIN AT NR 3 SLAT AFT INBOARD EDGE UP STOP PAD, RIB 15. MAINTENANCE REMOVED UP STOP PAD AND BLENDED OUT CRACK ON LT WING LEADING EDGE SKIN RIB 15; FABRICATED A REPAIR DOUBLER AND NEW REPLACEMENT UP STOP PAD; INSTALLED REPAIR PARTS IAW AWA ER 26-5721-00006-JS2.