As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HYDRAULIC SYSTEM NR 2 LOST ALL FLUID INFLIGHT. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP (EDP). PERMA SWAGGED PRESSURE LINE NR 2 SYSTEM AT ACCUMULATOR. RAN ENGINE AND ELECTRICAL PUMP. SERVICED SYSTEM. NO LEAKS NOTED. PERFORMED OPS CHECKS OF FLIGHT CONTROLS ASSOCIATED WITH NR 2 SYSTEM. OPS CHECKS GOOD.