As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RUDDER CONDUCTIVE FRAME PREVIOUS REPAIR SPLICE STRIP PEELED BACK; LH SIDE AT TE.<[01] INSTALLED NEW SPLICE STRIP AND VERIFIED CONDUCTIVITY LESS THAN 0.01 OHM IAW SRM 55-40-01-2R-2.;[02] NO CHANGE TO WEIGHT AND BALANCE. NO ADDITIONAL MATERIAL ADDED; MATERIAL INSTALLED EQUAL TO MATERIAL REMOVED.;[03] ADDED REFERENCE AND DAMAGE RECORD