As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING INBD FLAP, MOST INBD T/E UPPER SURFACE HAS A 2.5 " X .1 " X .002" CHAFE MARK. SMOOTHED & BLENDED CHAFE MARK IAW SRM 51-73-10 ORIGINAL THICKNESS OF .012 AFTER .008 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, FIG 101. R & R SKIN ASSY AT RT INBD FLAP T/E WEDGE IAW SRM 51-40-21 AND 51-72-10.