As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE NR 6 L/E SLAT WAS PUNCTURED ON ITS UPPER SURFACE, 16 OB FROM THE IB EDGE, AND 3 FWD OF THE TE. THE TE WEDGE IS MF FROM ALUMINUM HONEYCOMB WITH ALUMINUM FACESHEETS. THE TE WEDGE IS THE SUBJECT OF TWO AD'S, THEREFORE THIS ER/A WILL AUTHORIZE REPAIR.