What was found
(CAN) CREW REPORTED HYDRAULIC SYSTEM NR 2 EDP FAILURE AND FLUID LOSS. CREW FOLLOWED QRH PROCEDURE AND ELECTED TO RETURN TO FIELD. PART: ENGINE DRIVEN PUMP P/N: 848847 (TC# 20120126009)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CREW REPORTED HYDRAULIC SYSTEM NR 2 EDP FAILURE AND FLUID LOSS. CREW FOLLOWED QRH PROCEDURE AND ELECTED TO RETURN TO FIELD. PART: ENGINE DRIVEN PUMP P/N: 848847 (TC# 20120126009)