As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING REPAIR OF ADJACENT TAILCONE SKIN CRACKS A DETAILED VISUAL INSP OF THE UPPER RT HORIZONTAL STABILIZER SPAR REVEALED A CRACK RADIATING FROM A SINGLE STABILIZER ATTACHMENT FITTING, ATTACHMENT BORE AROUND THE SPAR'S FLANGE RADIUS AND ENDING AT A RIVET BORE UNDER THE TAIL CONE SKIN. OVERALL CRACK LENGTH 1.1 INCH.