As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING X-RAY INSPECTION OF THE VERTICAL STABILIZER, A CRACK WAS NOTED ON THE CENTER SPAR FLANGE LOCATED 2 FASTENERS UP FROM THE EXTERNAL DOUBLER APEX. THE CRACKIS APPROXIMATELY 5/8 - 3/4 INCH IN LENGTH AND RUNS 90 DEGREES TO THE FLANGE. A CRA CK APPROXIMATELY 1INCH IN LENGTH WAS DETECTED ON CHANNEL P/N 410008-85. THIS CRACK RUNS VERTICALLY UP THE RIGHT HAND FLANGE. THIS AREA IS COVERED BY AD 95-13-02. THE AIRCRAFT HAD BEEN MODIFIED IAW SB 208 PT2.