As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE NR 8 FLIGHT SPOILER ACTUATOR WAS FOUND STATICALLY LEAKING FROM THE INPUT LINKAGE ASSEMBLY. THE FLIGHT SPOILER WAS OPERATED WITH NO CHANGE TO THE LEAK RATE. THE ACTUATOR WAS REPLACED AND OPERATIONALLY CHECKED WITH NO LEAKS FOUND. THERE WAS NO MEASURABLE FLUID LOSS FROM THE HYDRAULIC SYSTEM.