As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A FUEL STOP, ENGINEER FOUND CRACK IN BLADE. NO ABNORMAL FLIGHT CHARACTERISTICS. CRACK RUNS FROM THE INBOARD CORNER OF THE TRIM TAB, FORWARD TO THE SPAR AND THEN INBOARD ALONG THE SPAR FOR 6 INCHES. BELL ASB 205-96-67 IS BEING DONE DAILY, BUT THIS CRACK IS NOT IN THE AREA COVERED BY THE ASB.