As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES HAVE NICKS ON THE LEADING EDGES.(<P>BLENDED OUT ENG NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES LEADING EDGES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION ON THE BLENDED AREAS. NO CRACK INDICATIONS NOTED AT THIS TIME REF 70-11-00 P1B 201</P>)