As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE INVESTIGATING THE CAUSE OF A BROKEN PITOT LINE WHERE THE WING MEETS THE FUSELAGE, EXCESSIVE MOVEMENT WAS NOTICED BETWEEN THE WING AND FUSELAGE. WHEN THE WING WAS REMOVED IT WAS DISCOVERED THAT THE FORWARD WING RIB P/N 95639-002 HAD CRACKED COMPLETELY AROUND THE FORWARD WING ATTACH POINT. FURTHER INVESTIGATION REVEALED THE AFT WING ATTACH POINT BOLT HOLE, AND MAIN SPAR BOLT HOLES HAD BEEN ELONGATED DUE TO THE ADDITION STRESS AND MOVEMENT.