As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON LANDING HYDRAULIC SYSTEM NR 1 QUANTITY WENT TO ZERO. PRESSURE LIGHT CAME ON FOR AIR PUMP AND ENGINE PUMP. TAXIED OFF RUNWAY AND WAS TOWED TO THE GATE DUE TO LOSS OF BODY AND NOSE LANDING GEAR STEERING. *S/D* LOSS OF HYDRAULIC FLUID WAS DUE TO CRACKED BODY/NOSE LANDING GEAR SELECTOR VALVE WHICH CAUSED THE ENGINE DRIVEN PUMP TO FAIL. REPLACED VALVE, ENGINE DRIVEN PUMP AND CASE DRAIN FILTER.