What was found
(CAN) TAKEOFF REJECTED DUE TO NR 1 ENGINE TORQUE FLUCTUATING BETWEEN 85-95 PERCENT. HYDRO MECHANICAL UNIT (HMU) TESTED, FAILED DELASTIC POTENTIOMETER TEST. HMU REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) TAKEOFF REJECTED DUE TO NR 1 ENGINE TORQUE FLUCTUATING BETWEEN 85-95 PERCENT. HYDRO MECHANICAL UNIT (HMU) TESTED, FAILED DELASTIC POTENTIOMETER TEST. HMU REPLACED.