As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, RIGHT WING UPPER REAR SPAR SIDE OF BODY SPLICE PLATE AREA NR 5 FASTENER HOLE FOUND CRACK AT INTERNAL SPLICE FITTING (CRACK LENGTH .25 INCH). RIGHT WING INTERNAL SPLICE FITTING BOLT HOLE NR 5 REPAIRED AS PER HX RS R57-18-35333 & UPS EO B747-5710-22476-A.