As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL OF THE LEFT WING LEADING EDGE SKIN, AN ELONGATED FASTENER HOLE WAS NOTED AT OSS 1017 THROUGH THE LEADING EDGE RIB AND THE UPPER LEADING EDGE SKIN PANEL SPLICE PLATE. THE ELONGATED HOLE WAS REAMED TO A TRUE AND ROUND CONDITION WITH A DIAMETER OF 0.4536” FROM A NOMINAL DIAMETER OF 0.309”.