As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE DENTED AT FRAME 5 BETWEEN STRINGER 35L & 36L. DENT MEASURES 1.4W X .025D & .5" FROM FRAME. REPAIRED AREA IAW SRM 53-00-41 FIG 232. SRI 53-00-11-2-017-00 REQUIRES FIRST INSP 60000C AFTER REPAIR EMBODIMENT. CURRENT CYCLES 23,653C.