What was found
ABORTED TAKEOFF AT LESS THAN 60 KNOTS DUE TO NR 1 ENGINE VIBRATION. THE HIGH PRESSURE COMPRESSOR EXPERIENCED A FIFTH STAGE BLADE FAILURE. THE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,471.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ABORTED TAKEOFF AT LESS THAN 60 KNOTS DUE TO NR 1 ENGINE VIBRATION. THE HIGH PRESSURE COMPRESSOR EXPERIENCED A FIFTH STAGE BLADE FAILURE. THE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,471.