As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAKEOFF ROLL WAS ABORTED AT 65 KNOTS DUE TO COMPRESSOR STALL ON NR 3 ENGINE. PERFORMED TEST OF COMPRESSOR BLEED VALVE IAW MM 75-30-3, FOUND NORMAL. CHECKED ON ENGINE RUN UP IAW MM 71-00, FOUND NORMAL OPERATION NO COMPRESSOR STALL NOTED.