As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE CHAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPAIR FOR CONDITION. REPAIRED IAW ENGINEERING DISPOSITION AND AIRCRAFT WAS RETURNED TO SERVICE.