As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB R/H SIDE SKIN PANEL IS DELAMINATED INTERNALLY (VIEWED THRU THE LIGHTNING HOLE IN THE AUX SPAR) BETWEEN THE AUX SPAR AND THE FWD SPAR BETWEEN APPROX RIB 1 AND RIB 3. REMOVED AND REPLACED VERTICAL STAB R/H SKIN PANEL IAW B757 SRM 51-40-02 AND BOEING DRWING 175N2001 REV B.