As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A CHECK INSPECTION FOUND TWO CRACKS ON CENTER EXTENDED LEADING EDGE AROUNG LOWER SKIN A STA XFS 304.000 RT. REPAIR DOUBLER AND ALUMINUM FILLER WER FABRICATED AND INSTALLED IAW EWO ATI 57-067. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.