What was found
(CAN) CRACK WAS DISCOVERED DURING DAILY INSPECTION. THE CRACK WAS LOCATED IN THE TAIL BOOM DOUBLER BELOW THE 42" GEAR BOX WHERE IT IS NOTCHED TO ACCOMMODATE THE VERTICAL FIN SPAR. IT WAS APPROXIMATELY 1" IN LENGTH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACK WAS DISCOVERED DURING DAILY INSPECTION. THE CRACK WAS LOCATED IN THE TAIL BOOM DOUBLER BELOW THE 42" GEAR BOX WHERE IT IS NOTCHED TO ACCOMMODATE THE VERTICAL FIN SPAR. IT WAS APPROXIMATELY 1" IN LENGTH.