What was found
(CAN) CRACK DETECTED VISUALLY IN WEB OF RIGHT ARM OF THE NR 1 ENGINE FORWARD MOUNT FITTING. THE ENGINE WAS REMOVED TO FACILITATE LAP JOINT MODIFICATION AND REMOVAL TASK CARD CALLS FOR INSPECTION OF ALL ENGINE MOUNTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACK DETECTED VISUALLY IN WEB OF RIGHT ARM OF THE NR 1 ENGINE FORWARD MOUNT FITTING. THE ENGINE WAS REMOVED TO FACILITATE LAP JOINT MODIFICATION AND REMOVAL TASK CARD CALLS FOR INSPECTION OF ALL ENGINE MOUNTS.