As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER FRAME (T/E HINGE RIB) WHERE RUDDER RIG PIN R-5 GOES THROUGH FEEL AND CENTERING FRAME, FIN STA 142-150. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5530-01445. A DIP WAS ISSUED TO PERFORM AT PERMANENT REPAIR AT THE EARLIER OF 500 HOURS OR THE NEXT MAINTENANCE CHECK WHERE THE USE OF THE RIG PIN IS REQUIRED, NOT TO EXCEED 12 MONTHS.