As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING SCHEDULED MAINTENANCE, BOTH CONTROL COLUMN BOBWEIGHT SUPPORT ARMS FOUND DAMAGED. ONE ARM WAS FOUND CRACKED .3750 INCH FROM THE TOP FLANGE AND .50 INCH FORWARD OF THE ATTACH BOLT CENTERLINE. THE OTHER ARM WAS FOUND DEFORMED 1.1250 INCHES FORWARD OF THE ATTACH BOLT AND WITH A SMALL .1250 INCH CRACK IN THE UPPER FLANGE.