As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT ATTACH CLIP; CRACKED THROUGH. / REMOVED & REPLACED CRACKED ATTACH CLIP R/H WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT IAW BOEING DWG # 115A2000 REV. - B; B737 SRM 51-40-02-0G0 A TAG # A93212.