As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON VERTICAL STAB AFT SPAR RUDDER COVE LOCATED JUST ABOVE RUDDER FAIRING PANEL LH SIDE ON SPAR CLIP, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED AND PRIMED BLENDED AREAS IAW TEXTRON FIELD REPAIR FR-680-0126-11911.