As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK AT RIVET IN LOWER FLANGE OF RT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1463 JUST FORWARD OF VERTICAL STABILIZER REAR SPAR PLANE. A REPAIR DOUBLER AND SPLICE WERE INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.