As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER ENGINE REMOVAL, THE ENGINE MOUNT WAS REMOVED FROM AIRCRAFT CLEANED AND INSPECTED. A CRACK IN THE WELD WHERE THE ANGLED PLATE IS WELDED TO THE TUBULAR TRUSS ADJACENT TO THE LOWER LEFT ISOLATOR MOUNT. THIS IS THE SECOND TIME A CRACK HAS BEEN FOUND IN THIS AREA.