As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE FIRST STAGE FAN BLADE NICKED ON LEADING EDGE APPROX 12 INCHES FROM OUTBOARD END WITH A DEPTH OF .010. ACCOMPLISHED FIRST BLEND ON BLADE IAW AMM 72-31-02. ACCOMPLISHED HFEC AS REQUIRED REF NDT MANUAL PART 6 72-31-401. NO CRACKS FOUND.