As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STIFFENER ON THE INTERIOR OF THE LT WING L/E AT PANEL 530DZ IS CRACKED. REMOVED DAMAGED EDGING FROM WING L/E WS 149.58 TO 247.95 IAW SRM 51-42-06 AND 51-42-13. DRILLED NEW PART IAW SRM 51-40-11. INSTALLED NEW EDGING ON LT WING L/E IAW SRM 51-42-13 AND 51-42-06 AND DWG NR PL601R12044.