As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT I/B AFT FLAP LEADING EDGE CRACKED AT 3RD HINGE OBD. REMOVED LEADING EDGE IAW SRM 51-40-02; CUTOUT DAMAGED PORTION IAW 57-53-01; FABED SKIN REPAIR AND SPLICE PLATE IAW 57-53-01; TREATED AND PRIMED REPAIR PARTS IAW 51-20-01; INSTALLED PARTS AND SEALED IAW 51-40-07 AND 57-53-01