What was found
(CAN) WHILE PERFORMING A CONTROL COLUMN INSPECTION DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE ELEVATOR BALANCE WEIGHT SUPPORT ARM. THE CRACK WAS LOCATED APPROXIMATELY 1 INCH FROM BOLT HOLE AT TORQUE TUBE END.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) WHILE PERFORMING A CONTROL COLUMN INSPECTION DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE ELEVATOR BALANCE WEIGHT SUPPORT ARM. THE CRACK WAS LOCATED APPROXIMATELY 1 INCH FROM BOLT HOLE AT TORQUE TUBE END.