As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAILCONE SLIDE DEPLOYMENT LANYARD WAS NOT LOOPED AROUND THE TAILCONE RELEASE MECHANISM CAM. DISCONNECTED THE LANYARD FROM CLEVIS AT THE SLIDE BOX AND RECONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM 25-62-01-201. INSPECTION OF LANYARD INSTALLATION WAS COMPLIED WITH (RII).