As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR, DURING ROUTINE MX A CRACK WAS FOUND ON THE RUDDER TRIM ROD CUT OUT. APPROX RUDDER STA CSS 31.20. CRACK APPROX .375 INCH LONG. MX REMOVED DAMAGED AND REPAIRED THE AFFECTED AREA IAW EO-09-1900-27-001. RII INSPECTIONS COMPLIED WITH AND RUDDER BALANCED IAW MM 55-40-00-201. NO WEIGHT CHANGE REQUIRED.