As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REAR SPAR CARRY THROUGH IS CRACKED.THE CRACK RADIATES FROM THE LOWER RIGHT MOST OUTBOARD FASTENER OF THE FUSELAGE REAR WING ATTACH FITTING. THE LENGTH OF THE CRACK IS APPROXIMATELY 5/16" AND CAN BE SEEN WITHOUT MAGNIFICATION. THE CRACK WAS CONFIRMED WITH EDDY CURRENT EQUIPMENT.