As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE FAN ROTOR BLADE 21 HAS DENT APPROX 5.5 INCHES FROM ROOT AREA AT LEADING EDGE. BLENDED NR 1 ENGINE FAN ROTOR BLADE 21 IAW M/M 72-31-02-801 SEE L/P 316815 ITEM 70. ACCOMPLISHED FLUORESCENT PENETRANT TEST OF NR 1 ENGINE, BLADE 21 PER AMM 70-11-06, NO CRACK INDICATION NOTED.