As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE 5 KM BETWEEN VS 55.625 PERCENT AND VS 67.5 PERCENT. SPAR DATUM BETWEEN STRINGER 2R AND 4R HAS A DENT 1.5 INCH LONG X 1.875 INCH WIDE X .109 INCH DEEP. REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN VS 55.625 AND VS 67.5 SPAR DATUM BETWEEN STRINGERS 2R AND 4R IAW EO. (K)