As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FRONT SPAR FORWARD TERMINAL PIN JOINT HOLE CRACKED AFT FORWARD. LEVELED AND SHORED A/C IAW SRM 51-50-1. CUT LOWER CHORD ANGLE AND WEB IAW BOEING DWG 65C29064. REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGLE IAW BOEING DWG 65C29064.