As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT ENGINE HAS A SIGNIFICANT NICK IN BLADE 2, BLADE DAMAGE IS AT DIM LEADING EDGE FROM BASE TO DAMAGE IS 20.700. APPROX 750. DEPTH AND LENGTH IS 1.0 INCH. PER MM DOCUMENT BLADE IS NOT REPAIRABLE. REPLACED NR 2 1ST STAGE FAN BLADE AND OPPOSITE FAN BLADE NR 21.