As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FIXED L/E IS CRACKED AT THE INBD OF SLAT DRIVE MECHANISM ACCESS PANEL. CUT OUT CRACKED AREA AND FABRICATED A DOUBLER AND FILLER IAW SRM 57-10-00; FIG 68; VOL I. ALODINED AND PRIMED THE DOUBLER AND FILLER IAW SRM 51-21-01; VOL II; PGS 21-24. INSTALLED THE DOUBLER AND FILLER IAW SRM 51-33-01; VOL II.