What was found
ON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LINE.