As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND TRAPPED WATER IN RUDDER LT SIDE PANEL TRAILING SCREW LINE. REMOVED OUTER SKIN AND CORE IN THE DAMAGED AREA MADE HONEYCOMB CORE PLUG PER SRM 55-41-12/201 FIG 222. DRIED THE REPAIR AREA AT 60 DEGREE FOR AT LEAST 20 HOURS PER SRM 51-77-10. INSTALLED HONEYCOMB CORE PLUG , SMOOTHED HONEYCOMB CORE PLUG, MADE THE OUTER SKIN DOUBLER, & RESTORED THE OUTER DOUBLER PER SRM55-41-12/201 FIG 222. RESTORED FINISH PER SRM51-75-10