As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ON LET DOWN #2 HYDRAULIC SYSTEM LOST FLUID. ON LANDING ROLL AT 60 KTS BRAKE PEDALS WENT TO THE FLOOR DUE TO FLUID LOSS. BOTH QUANTITY GAUGES SHOWED EMPTY. LINE FROM ANTI-SKID VALVE TO QLV ON #1 SYSTEM FOUND CRACKED. #2 SYSTEM GROUND SPOILER BLANKING CAP FITTING FOUND LOOSE AND O-RING DAMAGED.