As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C2 CHECK - AREA OF DISBONDING ON SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER TORQUE BOX BETWEEN FSS 150 TO FSS 180 & BETWEEN ASS 0 TO FSS 0. REPLACED SKIN PANEL ON LOWER RIGHT SIDE OF VERTICAL STABILIZER IAW B757 SRM 51-40-02.