As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C3 CRACKED UPPER RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE. STOP DRILLED CRACK ON UPPER RIB INSIDE PANEL 518A LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002. FABRICATED AND INSTALLED ANGLE DOUBLER ON RIB INSIDE PANEL 518A ON LEFT WING OUTBOARD LEADING EDGE IAW SRM 57-02-00 FIG 002, AND SRM 51-1-20D.