As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING "A" LEVEL INSPECTION, CORROSION WAS FOUND ON THE RT WING MAIN INBOARD FLAP FOLLOW UP CABLE AT THE END SWEDGE FITTING. WHILE CHECKING THE INTEGRITY IF THE CABLE IN THE FITTING, THE CABLE COMPLETELY SEPERATED FROM THE FITTING. THE RIGHT WING FLAP CABLE WAS REPLACED AND RIGGED. FLAP SYSTEM OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE.