As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON THRUST REDUCTION TO CLIMB, NR 2 ENGINE HAD TWO COMPRESSOR STALLS BEFORE THRUST LEVER COULD BE MOVED TO IDLE. EGT EXCEEDED LIMITS; ENG 2 FAIL ON ECAM. NR 2 ENGINE WAS SHUTDOWN IAW ECAM ACTIONS, FIRE BOTTLE WAS DISCHARGED AND AIRCRAFT DIVERTED, (EMERGENCY DECLARED). MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. FOUND THE BLEED VALVE MASTER ACTUATOR FAILED DUE TO HIGH LEVELS OF FUEL LACQUER ON PISTON AND LINER ASSEMBLIES AND TORQUE MOTOR FILTERS.