As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING INBD FLAP FWD L/E PANEL IS CHAFED AT THE OUTBD HINGE AREA. BLENDED CHAFFED AREA & FOUND OUT OF LIMITS IAW SRM 57-00-01 VOL I, ORIGINAL THICKNESS 0.080. REMAINING MATERIAL 0.020. MATERIAL REMOVED 0.060. FABRICATED SKIN & INNER DOUBLER IAW DWG ARC 3152, REV M. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. REMOVED & REPLACED SKIN PANEL IAW SRM 51-31-01 VOL II. PAINTED SKIN PANEL IAW SRM 51-21-01 VOL II.