As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY REPIAR TO INTERIOR RIB CROSS SUPPORT ANGLE PER SRM 51-40-8 FIG 1. INSTALLED RIB SUPPORT ANGLE PER SRM 51-30-2.