As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AN EXISTING REPAIR ON THE L/E OF THE NR 3 LT FLAP OB FOUND TO BE CRACKED ADJACENT TO THE INSERT REPAIR. CRACK IS 1 INCH IN LENGTH AND STARTS AT THE LOWER EDGE OF REPAIR COUTOUT GOING DOWNWARD. CARRIED OUT PERMANENT REPAIR IAW SRM USING SOLID FASTENERS. PREVIOUS REPAIR 48 INCHES IB OF OB END. (K)