As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE CREW REPORTED THAT THE HYDRAULIC CONTROL CIRCUIT BREAKER TRIPPED DURING GEAR RETRACTION, RESET BREAKER, HYD PUMP FUNCTIONED NORMALLY. DIVERTED SAFELY. INSPECTED HYD PACK/MOTOR AND ASSOCIATED COMPONENTS IAW AMM CH: 29-00-00 WITH NO DEFECTS NOTED. INSPECTED ALL LANDING GEAR & ASSOCIATED WIRING, SWUNG GEAR SEVERAL TIMES IAW AMM 32-00-00 WITH NO DEFECTS NOTED.