As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING REAR SPAR, OUTBOARD FLAP OUTBOARD DEFLECTION FITTING CRACKED. THE SUBJECT FITTING CRACKED TO CYCLICAL FATIGUE LOAD DURING EXTENSION AND RETRACTION OF THE OUTBOARD FLAP. CORRECTIVE ACTION IS REPLACEMENT OF THE FITTING WITH NEW AND IMPROVED FITTING PER COA 616463.