As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON TAKEOFF ROLL C&W PANEL ENGINE VIBRATION FILTER PRESS LIGHT ON NR 3 ENGINE INDICATING 2.6 UNITS FAN POSITION. ABORTED TAKEOFF AT 80 KNOTS POWER SETTING .427 EPR. CHECKED CHIP DETECTORS AND MAIN OIL SCREEN, ALL OK. LUBED BLADES IAW MM 72-31-05, PERFORMED TEST 11 VIBRATION SURVEY WITHIN LIMITS IAW MM 71-91-00. BOROSCOPE DEFERRED FOR 25 HRS IAW 71-00-00.