As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFE DAMAGE TO THE LOWER WING SKIN PANEL # 1 (P/N: 111T4015-4) AND LOWER CENTER WING BEAM (LBL 62.05) WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE CHAFE AREA COMMON TO THE LOWER CENTER WING SKIN PANEL # 1 MEASURED WERE APPROXIMATELY 1.25" (CHORDWISE) X 0.049 (DEPTH). THE SKIN, WING BEAM WEB, DOUBLER, AND LOWER CHORD WERE REPAIRED. THE AIRPLANE WAS GROUNDED.