As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE FAN BLADE NR 1 HAS DAMAGE ON L/E. INSPECTED AND BLENDED NR 2 ENG NR 1 BLADE APPROX 1" FROM TIP PER MM 72 21 02 300 801 F00. PERFORMED FLUORESCENT PENETRANT INSP & FOUND NO DEFECTS NOTED REF MM 70 40 01 230 801 F00 & ASA NODT MANUAL SEC 5 6.