As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFE MARK LEADING EDGE OF RIGHT OUTBOARD MAIN FLAP INBOARD SIDE. REMOVED DAMAGE ON LEADING EDGE OF RT OUTBOARD MAIN FLAP INBOARD SIDE, IAW B757 SRM 51-10-02. ORIG MAT .080 REM .030 LOSS .050 FOUND TO BE OUT OF LIMITS, IAW B757 SRM 57-53-01-1A FIG 101. REPAIRED FLAP IAW B757 SRM 57-53-01-2R RP 5 FIG 201.