As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS GOUGED AND DENTED JUST ABOVE THE LAP JOINT AT S-24L AT FS 268. WHILE REMOVING THE DAMAGE TO THE FUSELAGE SKIN, THE STRINGER 24L INCURRED TOOLING DAMAGE. A STRINGER REPAIR AND AN EXTERNAL SKIN REPAIR WERE INSTALLED PER 460778-14.