As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK SUPPORT ANGLE ON BODY FAIRING STRUCTURE BS 500D LEVEL STRINGER 19L AT LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AT WING TO BODY FAIRING STRUCTURE BSTA 500D AT LEVEL OF STRINGER 19L. LOWER FUSELAGE. IAW SRM 51-40-02 . SRM 51-10-02 PARAGRAPH 9. AND DWG 116A3010. SHEET 33. REV. C.