As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C6 CHECK - RT SLAT LOWER T/E IS CHAFED INTO PANEL 622CB. BLENDED CHAFE DAMAGE, PERFORMED FPI ON AREA IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. SENT ENGINEERING REQUEST TO MFG. RECEIVED ENGINEERING REO 670-57-42-288, AREA IS OK AS BLENDED. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.