As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - PILOTS REPORTED THAT THE FUSELAGE WAS PUNCTURED IN THE LT FUSELAGE JUST FWD OF FS 273.25 ON THE UPPER SKIN. DAMAGED AREA APPROX 2.1 INCH BY 3.5 INCH. (2) CRACKS PRESENT. (1) CRACK APPROX 2.3 INCHES AND THE OTHER 1.1 INCH IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-020. RII INSPECTION C/W IAW EO 09-1900-53-020.