As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF LEFT MAIN GEAR WELL AREA FOUND WING ATTACH FITTINGS TO HAVE VERTICAL CRACKS APPROXIMATELY .50 INCH IN LENGTH BETWEEN RIVETS THAT ATTACH FITTING TO SPAR. THESE CRACKS ARE LOCATED IN THE WEB/RADIUS AREA OF THE FITTING ANGLE.