As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TRUSS MOUNT CRACKED AT TUBE THAT ATTACHES THE REAR UPPER ENGINE MOUNT. THIS MOUNT WAS WELDED UNDER THE LUG POINT AND WAS NOT EFFECTED BY THE CALL OUT OF SB 227-71-008. FIRST WELDED ONE SUBMITTER HAS SEEN CRACKED. PRIOR CRACKS HAD BEEN THOSE NOT WELDED.