What was found
DURING A SCHEDULED ENGINE CHANGE AN INSPECTION OF THE LEFT ENGINE MOUNT TRUSS REVEALED A .500 INCH CRACK IN THE UPPER INBOARD FORWARD TUBE AT THE UPPER INBOARD FORWARD TUBE INTERSECTION WELD. THE CRACK WAS REPAIRED BY WELDING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ENGINE CHANGE AN INSPECTION OF THE LEFT ENGINE MOUNT TRUSS REVEALED A .500 INCH CRACK IN THE UPPER INBOARD FORWARD TUBE AT THE UPPER INBOARD FORWARD TUBE INTERSECTION WELD. THE CRACK WAS REPAIRED BY WELDING.