As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: DAMAGED INTERNAL HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE CUTOUT. NEW HARDWARE ON LEVER OF THE TAIL CONE JETTISON MECHANISM AT RT LOWER CORNER OF THE TAILCONE WERE INSTALLED PER AMM TAILCONE ADJUSTED WAS PERFORMED AND TEST OK PER AMM 53-52-01-830-802. (LP1155413)