As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING ROOT REAR SPAR BOTTOM SKIN FOUND ONE EACH FASTENER HEAD POPPED OUT. REMOVED THE HEAD POPPED OUT FASTENER IAW SRM 51-40-21. CARRIED OUT ROTOTEST INSPECTION TO FASTENER HOLE IAW NTM 51-10-18, FOUND CRACK. REAMED THE HOLE TO REMOVE CRACK IAW SRM 51-40-44. FURTHER OVERSIZED THE DISCREPANT HOLE BY REAMING ALL LAYERS TO 15.836-15.876MM. WET INSTALLED WITH FASTENER NSA 5350-10 IAW EA 6-5710-T0317253. MAJOR REPAIR IAW GMM 6-2-100.