As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND ON STIFFENER ON INTERIOR OF RT WING L/E AT ACCESS PANEL CUT-OUT 630CZ. REMOVED DAMAGED EDGING/STIFFENER FROM RT WING LOWER L/E. DRILLED UP NEW PART IAW SRM 51-40-11. INSTALLED NEW EDGING ON RT L/E IAW SRM 51-42-13 AND 51-42-06 AND DWG NO PL601R12044.