As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER LT SIDE 8 INCHES BELOW TIP, 4 INCHES FWD OF T/E FASTENER HEAD POPPED, POSSIBLE DELAMINATED. REMOVED RUDDER TIP PANEL, REPLACED RUDDER TIP FITTING, REPLACED RUDDER TIP PANEL IAW SRM 51-40-02 AND SEALED IAW 51-20-5. ACFT WAS GROUNDED.