As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVING CONDUCTIVE STRIP; FOUND FASTENER HOLES ELONGATED AND DAMAGED ON RH O/B UPPER AND LWR HORIZ. STAB T/E SKIN SURFACE AT STA 281 HOLE #1; HOLE #8 AND HOLE 13 FROM O/B EDGE OF THE PANEL (MARKED) ON T/E / R&R 3 FASTNERS ON R/H HORIZ. STAB. TE PER SRM 51-40-02 REF. BOEING DRAWING H185A1800