As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FORWARD TAIL CONE FAIRING IS DELAMINATED, BS 1190 21 INCHES RIGHT OF TOP. CRACK LENGTH: L=2.3' W=2.2'. LOCATED & DRILLED INITIAL TAIL CONE SCREW HOLES WITH EXCEPTION OF HOLES AROUND ELEVATOR PUSH ROD CUT OUTS IAW MM 51-40-02 & SIP. TAIL CONE WAS R & R WITH A NEW ONE.