As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING NORMAL GEAR RETRACTION AT 170KTS HYD SYS NR 3 FAILED. FLUID QTY RAPIDLY DECREASED TO ZERO, OCCURRED WHILE USING RMP'S TO PRESSURIZE HYD SYS NR 3. ENG NR 3 PUMPS WERE SELECTED OFF. GEAR HAD BEEN CYCLED 5 TIMES PRIOR TO THIS FAILURE WITH NO PROBLEM. R & R HYD TRIM FUSE BLED NR 3 SYS & TRIM CYLINDER. PERFORMED GEAR SWING INCLUDING ALTERNATE EXTENSION & RETRACTION. ALL SYS CHECKED NORMAL, NO LEAKS NOTED. SUBSEQUENT TEST FLIGHT TESTED GOOD.