What was found
(CAN) IN FLIGHT LOSS OF HYDRAULIC PRESSURE ON THE GAUGE. AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND A 4" CRACK ON THE TOP OF THE HYDRAULIC PUMP. THE PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) IN FLIGHT LOSS OF HYDRAULIC PRESSURE ON THE GAUGE. AIRCRAFT RETURNED TO BASE. POST FLIGHT INSPECTION FOUND A 4" CRACK ON THE TOP OF THE HYDRAULIC PUMP. THE PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.