As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT UPPER CORE COWL IS CHAFED ON INNER FWD SIDE. BLENDED CHAFED AREA ON RT UPPER CORE COWL FWD SIDE AND REPAIRED IAW CMM 71-12-200-802-A01, MATT LOSS .002 MAT REMAINING .028. REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW CMM 71-12-200-802-A01.