As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A DRILL START WAS ERRONEOUSLY MADE TO THE FUSELAGE SKIN NEAR THE LOWER FORWARD CORNER OF THE L1 DOOR CUTOUT. THE AREA OF SKIN WITH THE DAMAGE WAS TRIMMED OUT. THE TRIM OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 093358-14, REV A.