As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS PUNCTURED APPROXIMATELY FIVE FEET AFT OF L-1 DOOR SILL. THE PUNCTURED AREA OF SKIN AND DOUBLER WERE CUT OUT IAW SRM 53-30-3. A REPAIR DOUBLER, FILLER, AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, AND 51-30-2.