As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE COMPLETING A X-RAY INSPECTION ON THE VERTICAL STABILIZER, A CRACK WAS NOTED ON THE RT VERTICAL FLANGE OF THE CHANNEL. THE CRACK IS APPROXIMATELY .6250 INCH IN LENGTH. IT IS LOCATED IN THE AREA COVERED BY AD95-13-02. THE AIRCRAFT HAD BEEN MODIFIED IAW SB218 PT2.THE AIRCRAFT WILL BE REPAIRED PRIOR TO BEING RETURNED TO SERVICE.