As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING EXT ZONAL INSP OF ACFT TAIL CONE, FOUND CRACKED IN (DOUBLER/STRAP) L/H SIDE FUSELAGE. TOP/FWD INTERSECTION OF TAIL CONE AND REAR SPAR DATUM (67.5%) AND VERTICAL STABILIZER. REPAIRED FWD AND AFT DRAG ANGLE ON L/H SIDE FUELAGE, TOP/FWD INTERSECTION OF TAIL CONE AND REAR SPAR DATUM AND VERTICAL STABILIZER IAW SRM AND REO.