As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT AFT FUSELAGE HAS PUNCTURE IN UNPRESSURIZED SKIN JUST BELOW SKIN LAP AND JUST FWD OF STAB COMPT ACCESS DOOR. DAMAGE WAS CUT OUT AND DOUBLER INSTALLED PER EVA 60177. A 8100-9 RECEIVED FROM BOEING. DTA INFORMATION TO FOLLOW FROM BOEING.