As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON INSPECTION OF TAIL BOOM, UPPER ATTACHMENT FITTING, IAW AD 2013-25-10 FOUND A CRACK THAT RAN ALL THE WAY ACROSS THE ATTACHMENT FITTING ON ONE SIDE THROUGH TWO RIVETS. THE RIVETS ARE THE TWO FWD MOST ON THE LOWER SIDE OF THE FITTING. CRACK APPEARS TO GO ALL THE WAY THROUGH THE METAL.