As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK CHAFE ON L/E OF FLAP PANEL 584EB. BLENDED CHAFED DAMAGE IAW SRM 51-12-00-001-001-A01. FOUND BLEND TO BE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. TREATED, PRIMED, TOP-COATED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-001-A01.