As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABORTED TAKEOFF AT 90 KNOTS DUE TO NR 1 ENGINE WOULD NOT MAINTAIN 100 PERCENT POWER OF 85 PERCENT TORQUE. EGT READ 650 THEN BYPASS LIGHT AND LOSS OF APPROXIMATELY 30 PERCENT TORQUE. ADJUSTED TORQUE SIGNAL CONDITIONER, RECOMPED FROM +3 TO -10. PERFORMED MAXIMUM POWER RUN, OPERATIONAL CHECKS GOOD.