As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#2 PRESSURE AND RETURN MANIFOLD CHANNEL CRACKED THROUGH BOLT HOLE. FOUND DURING C CHECK INSPECTION. FITTED AND INSTALLED NEW CHANNEL IAW SRM 51-40-11, 51-42-06. RE-INSTALLED HYDRAULIC COMPONENTS IAW CRJ MM CH. 49-11-05. P/N: 600-75221-130