As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMP T/C SBCFM56-7B-72-1033-1, FAN BLADE ROOT ULTRASONIC INSPECTION FOUND BLADE NR 3 S/N DD453914-J 32% INDICATION 5.25" FROM LE CONVEX SIDE. BLADE NR 11 S/N DD454177-5 31% INDICATION 1.25" FROM LE CONVEX SIDE. ALL BEYOND 30% REJECT, ENGINE NR 2 S/N 894276. GROUNDED - YES. REPLACED NR 2 ENGINE FAN BLADES NR 3 & NR 11 AND THEIR PAIR NR 15 & NR 23 PER AMM 72-21-02-000-802 & T/C 78472010.