As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE RIGHT FWD FUSELAGE II, CENTRAL FUSELAGE I SKIN AND SEVERAL UNDERLYING STRUCTURAL MEMBERS WERE DAMAGED AS A RESULT OF A TUG STRIKING THE AIRCRAFT. THE DAMAGE IS CONTAINED BETWEEN FRAMES 7 & 14, STR 16R & 20R. THE A/C IS BEING REPAIRED IAW EA5330-01106.