As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOSS RIGHT ENGINE HYDRAULIC PUMP INFLT FOLLOWED BY LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER M/M 29-10-5. RESERVICED RIGHT HYDRAULIC RESERVOIR AND INSTALLED TEMPORARY FLEX LINE ABOVE RIGHT THRUST REVERSER CONTROL VALVE. LEAK CHECKED AND OPS CHECK C/W. NO DEFECTS NOTED.