As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER PERFORMING A VISUAL INSPECTION ON THE RIGHT WING, DAMAGE WAS NOTED ON THE FITTING. FOUND THAT WHEN THAT AIRCRAFT FUSELAGE IS FIXED THE RIGHT WING EXHIBITED LEAD & LAG PLAY ABOUT THE MAIN SPAR. THE AMOUNT OF PLAY EXCEEDS THAT OF THE OPPOSITE WING. IAW MM THE BOLT WAS REPLACED. ASSOCIATED NUT AND WASHERS WERE ALSO REPLACED.