As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 2 INCH CRACK IN LT SIDE OF UPPER RUDDER LOWER TRAILING EDGE (JUST OUTBOARD OF TAB HINGE) AREA. THE HINGE FITTING WAS REMOVED FOR ACCESS, THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-40-2. THE HINGE FITTING WAS REINSTALLED.