As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE SPEED PARAMETERS EXCEEDED FOR LEFT ENGINE DURING TAKEOFF ROLL. PERFORMED BORO INSPECTION OF THE NR 1 ENGINE IP COMPRESSOR IAW MM 72-00-00-206-147-R02, AND IP TURBINE INSPECTION IAW 72-00-00-206-173-R02. NO DEFECTS NOTED. REMOVED AND REPLACED LEFT AND RIGHT BLEED VALVE SOLENOID IAW AMM 75-32-03.