As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE. REPLACED NEW ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE IAW SRM 51-40-02-0G-0 AND DWG 116A3110 SHEET 8 REV -; DWG 116A3010 SHEET 33 REV C; DWG-149A7101 SHEET 7 REV -.