As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK LEADING EDGE SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER (1 EA) / REPLACED SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 176A3001; MATERIAL USED P/N 2024-T0/0.040' P.O 2012-545964. CONVERTED FORM T0 TO T42