As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING T/E UPPER SURFACE OF THE MOST INBD FIXED PANEL AFT EDGE HAS CHAFING WEAR ABOVE THE INBD FLAP VANE INBD EDGE. TRIMMED WORN EDGE IAW SRM 57-00-01. REPAIRED PUNCTURED AREA BY BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. REMOVED CORROSION, ALODINED & PRIMED IAW 57-00-01 VOL I. CHECKED DENTS ON THE UPPER & LOWER SURFACES AND FOUND THEM TO BE WITHIN LIMITS IAW SRM 51-71-00 VOL II.