As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C-2 NLG W/W STA 400 S-44R SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6 51-00-00 FIG 1. CRACK FOUND AT AFT HOLE AT SPLICE FITTING, BUT NIL CRACK AFTER AFT HOLE REF SCATCH ON CWS 330869. EXISTING REPAIR DOUBLER REINSTALLED AS PER SRM 51-30-02.