As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AUTO FEATHER FAILED TO ARM ON TAKEOFF ROLL. ABORTED TAKEOFF. PERFORMED FUNCTION TEST OF POWER LEVER LIMIT SWITCHES, AUTO FEATHER ARMING INITIATES WITHIN TEST CHART OF DHC AMM 61-26-00, FIGURE 501. NO FAULTS FOUND. NO PARTS REPLACED, AIRCRAFT RETURNED TO SERVICE.