As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT INBD MAIN FLAP UPPER OTBD PANEL HAS CHAFE DAMAGE 0-36" FROM THE OTBD END. ACCOMPLISHED REPAIR, DAMAGE DIMENSION IS APPROXIMATELY 1" X 11" OF THE DISCREPANT AREAS ON LT INBD MAIN FLAP UPPER OTBD PANEL IAW ER/A 514121-14MA, ORIGINAL REVISION.