As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DEFLECTOR CHAFED ON RETAINER UNTIL IT SEPARATED COMPLETELY AND WAS LOOSE BETWEEN 2ND STATOR AND 2ND STAGE TURBINE WHEEL, MOVED INTO CONTACT WITH 2ND STAGE TURBINE WHEEL BLADE FIR TREE. RUBBED GROOVE IN BLADE FIR TREES. IF UNDETECTED, THIS CONDITION COULD RESULT IN ROTOR BLADE FAILURE - CATASTROPHIC ENGINE FAILURE. TOTAL CYCLES, 3,550.