As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) AFTER LANDING CREW EXPERIENCED A HYDRAULIC SYSTEM FAILURE NECESSITATING A TOW FROM THE RUNWAY TO THE GATE. SPECIFICALLY: ON TOUCH DOWN, SPOILER FAULT THEN HYDRAULIC 2 LOW QUANTITY . FOUND 3 BOLTS SHEARED ON RT NR 5 SPOILER ACTUATOR CASE. NR 5 RT MFS PCU REPLACED AS PER 27-65-01. LEAK & FUNCTION CHECKS SATISFACTORY.