As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON ROTATION, NR 2 REVERSER UNLOCK AMBER LIGHT ILLUMINATED WITH ECAM AND THRUST REVERSER PRESSURIZED ON ECAM. COMPLIED WITH ECAM AND QRH THRUST REVERSER UNLOCKED. ENG REVERSER UNLK PROCEDURE LIGHT AND ECAM REMAINED UNTIL SHUTDOWN. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. FOLLOWING MOCC MTSI, AND FIM 78-31-30, R & R THE NR 2 ENGREVERSER PRESSURE REGULATOR VALVE PER MM 78-31-05-04. CW NR 2 REVERSER TEST IAW MM 78-31-00-02. UNABLE TO DUPLICATE FAULTS. ALSO RAN ENG NR IAW JRH AT IDLE. ALL REVERSER SYSTEM IS WORKING FINE. ALL CHECKED OK.