As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE IS LEAKING OIL. LEAK TRACED TO RIGHT THRUST REVERSER HALF CENTER ACTUATOR OF THRUST REVERSER. NR 2 ENGINE THRUST REVERSER DEACTIVATED AS PER AMM 78-00-00-040-802-N00. OPERATED THE REV SIX TIMES, INSPECTED ALL ACTUATORS. NO SIGN OF LEAKS. REV OPS NORMAL.