As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A SPLIT FLAP CONDITION OCCURRED ON FINAL APPROACH. AFTER CHECKING SYSTEM, ALL CABLES WERE REMOVED FROM AIRCRAFT FOR REPLACEMENT. INTERNAL CABLE WEAR WAS FOUND AT ALL PULLEY LOCATIONS. HIGH CABLE SYSTEM TENSION IS REQUIRED ON THESE CABLES. SUBMITTER SUGGESTS LIFE LIMIT.