As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING MAIN SPAR CRACKED IN TWO LOCATIONS, ADJACENT TO THE DOUBLER FOR THE WING STRUT ATTACH FITTING. TOP EDGE OF SPAR CRACKED AT INBOARD AND OUTBOARD ENDS OF DOUBLER PLATES. LAMINATED SPAR, COMPRESSION CRACKS STOPPED AT GLUE JOINT OF TOP LAMINATION, ABOUT 1.5 INCHES THICK.