As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C1 AT FULL RIGHT THROW, RUDDER STRIKES TAIL CONE SKIN AT LEFT SIDE. REMOVED LEFT SIDE FLANGE OF RUDDER BOTTOM PANEL IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR PANEL AT LEFT RUDDER SKIN FLANGE IAW DWG 565507A AND SRM 51-1-20D.