What was found
(CAN) ON INSPECTION A CRACK ABOUT .0625" WAS FOUND COMING OUT OF A BALANCE WEIGHT SCREW HOLE ON THE NR 2 BLADE SOCKET ON THE CYLINDER HUB HALF.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) ON INSPECTION A CRACK ABOUT .0625" WAS FOUND COMING OUT OF A BALANCE WEIGHT SCREW HOLE ON THE NR 2 BLADE SOCKET ON THE CYLINDER HUB HALF.