As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE STEEL TUBE CRACKED .50 INCH FROM AFT WELD LOCATION. CRACK SEPARATION WAS APPROXIMATELY .25 INCH WIDE THROUGH THE TUBE. CRACK WAS DETECTED DURING AN ANNUAL INSPECTION. TUBE ALSO HAD A NOTICEABLE DOWNWARD BEND MID-POINT OF THE TUBE. THE BEND IS APPROXIMATELY .50 INCH DEEP, 6 INCHES IN LENGTH.