As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, BS 1241 LT WING REAR SPAR UPPER SPLICE FITTING FOUND CRACKS AT HOLE NR 5. BS 1241 LT WING REAR UPPER SPLICE FITTING HOLE NR 5 REAMED TO REMOVE CRACKS. HFEC INSPECTED RESULT CRACK FREE. FINAL HOLE DIAMETER IS 1.000 INCH AND BUSHING INSTALLED AS PER EO B747-5740-17032-A APPENDIX -E-.