As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 2 BOWED ROTOR PROTECTION FAULT DISPLAYED. // PERFORMED EEC SYSTEM TEST PER AMM 73-21-00. TEST OK. PERFORMED EEC RESET TO CONFIRM IF ACTUAL FAULT. MESSAGE CLEARED. CONTACT PRATT & WHITNEY REP. PERFORMED IDLE ENGINE RUN FOR 5 MUNITES PER AMM 71-00-00-860-823-A & 71-00-00-720-811-A. NO ECAM FOR ENG 2 BOWED ROTOR PROTECTION FAULT. OK FOR SERVICE.