What was found
CRACK LEADING EDGE ON SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER / REPLACED SUPPORT ANGLE LOC INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING # 176A3101 REV -
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK LEADING EDGE ON SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER / REPLACED SUPPORT ANGLE LOC INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING # 176A3101 REV -