As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A CRACK INDICATION IN NR 2 HOLE OF LT WING REAR SPAR UPPER CHORD AT GEAR BEAM CASTING ATTACH POINT. THE HOLE WAS REAMED AND THE CRACK WAS FOUND TO EXCEED 0.500 INCH MAX REAM LIMIT. THE REAR SPAR UPPER CHORD WAS REMOVED AND REPLACED FROM INBOARD END TO RSS 284 USING A SPLICE REPAIR IAW ECRA 5720-01855 AND ECRA 5360-01059.