As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CRACK FOUND ON THE FUSELAGE TO TAILBOOM ATTACHMENT FLANGE. CRACK LOCATED (LOOKING FORWARD) AT 2:30 POSITION ON RIGHT SIDE. CRACK LENGTH WAS APROXIMATELY 3.5 CM LONG AND ABOUT 2 MM FROM EDGE. THE TORQUE ON FUS/TAILBOOM ATTACH BOLTS WERE UNKNOWN AT THE TIME OF TAILBOOM REMOVAL (RE: CF-93-12R1).