As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON T/O ROLL, NR 3 ENG INSTR WERE UNSTABLE. ABORTED AT 110 KNOTS. ON INITIAL PWR APPLICATION NR 3 ENG WAS STABLE THEN PROGRESSIVELY BECAME UNSTABLE. NORMAL PWR USED. VERSA LUBE NR 3 ENG FUEL CONTROL. INSP MAIN CHIP DETECTOR, INSP INTAKE, EXH AND NO DEFECTS FOUND. RAN PFHB, ALL IND NORMAL.