What was found
(CAN) #1 HYDRAULIC SYSTEM WENT TO ZERO QUANTITY ON APPROACH. THE RIGHT INBOARD SPOILER DUMP VALVE AT ACTUATOR LINE HAD CRACKED AT RADIUS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) #1 HYDRAULIC SYSTEM WENT TO ZERO QUANTITY ON APPROACH. THE RIGHT INBOARD SPOILER DUMP VALVE AT ACTUATOR LINE HAD CRACKED AT RADIUS.