As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE DAILY INSP IT WAS NOTED THAT THE UPPER LT CAP ANGLE HAS A CRACK IN THE VERTICAL LEG AT THE FWD END OF THE TAILBOOM ATTACH FITTING PN 212-030-159-001. IAW AD2000-18-09 AND ASB 412-00-100 THE CAP ANGLE MUST BE REPLACED BEFORE FURTHER FLIGHT.