As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 CENTER WING EXTERIOR FUSELAGE -L- ANGLE CRACKED AT ST 857.125 RBL 65. REMOVED CRACKED -L- ANGLE AT STA 857.125 RBL 65 IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR -L- ANGLE AT STA 857.125 RBL 65 IAW DWG 5649893, AND SRM 51-01-20D.