As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PANEL 684ET CHAFED. (C-CHECK) RO 6/21/2020 BLENDED OUT DAMAGE FLAP PANEL 684ET REF SRM. ORIGINAL MATERIAL THICKNESS .050" REF SRM. REMAINING THICKNESS .030". MATERIAL LOSS .020". MAX MATERIAL LOSS ALLOWED .010" (20%). FOUND TO BE OUT OF LIMITS REF SRM. ORDERED AND RECEIVED REPLACEMENT PANEL 684ET PART CC670-14027-3 AND LOCATED HOLES IN REPLACEMENT PANEL REF SRM. RESTORED FINISH REF SRM.