What was found
HYD SYS 2 AT 0% DURING FLIGHT / PERFORMED INSPECTION OF THE ENGINE DRIVEN PUMP (EDP) AFTER OPERATION WITHOUT HYDRAULIC FLUID IAW AMM 05-51-33-210-801-A01 AND FOUND LEAK ON ENGINE DRIVEN PUMP, EDP, CASING. REMOVED AND REPLACED RT ENG ENGINE DRIVEN PUMP,EDP, IAW AMM 29-11-01-000/400-801-A01-PSA. PERFORMED BLEEDING OF NR 2 HYD SYSTEM IAW AMM 29-10-00-870-801-A01, FUEL AND OIL LEAK CHECK IAW AMM 71-00-00-790-807-A01,FUNCTIONAL CHECK OF EDP IAW AMM 29-11-01-720-801-A01 AND OPS TEST OF THE HYDRAULIC EDP SOLENOID CIRCUITRY WITH MDC IAW AMM 29-11-01-710-801-A01. ALL CHECKS GOOD AND NO LEAK NOTED.