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 CRACK IN (DOUBLER/STRAP) R/H SIDE FUSELAGE. TOP/FWD INTERSECTION OF TAIL CONE AND REAR SPAR DATUM (67.5%) AND VERTICAL STABLIZER. REPAIRED FWD AND AFT DRAG ANGLE ON R/H SIDE FUSELAGE, TOP/FWD INTERSECTION OF TAIL CONE AND REAR SPAR DATUM AND VERTICAL STABLIZER IAW SRM.