As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE FLEX LINE LEAKING. THE LINE WAS REPLACED WITH A SOLID LINE. THE HYDRAULIC RESERVOIR WAS SERVICED, LEAK AND PRESSURE CHECKS WERE GOOD.