What was found
(CAN) #2 HYDRAULIC SYSTEM LOST ALL HYDRAULIC FLUID DURING FLIGHT. POST FLIGHT INVESTIGATION FOUND "O" RING AT #2 ENGINE DRIVEN HYDRAULIC PUMP DETERIORATED CAUSING LEAK OF ALL FLUID.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) #2 HYDRAULIC SYSTEM LOST ALL HYDRAULIC FLUID DURING FLIGHT. POST FLIGHT INVESTIGATION FOUND "O" RING AT #2 ENGINE DRIVEN HYDRAULIC PUMP DETERIORATED CAUSING LEAK OF ALL FLUID.