As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF AT MAX POWER 1.87 GPR BETWEEN 60 AND 80 KNOTS, HAD A LOUD BANG ON NR 2 ENGINE COMPRESSOR N2 INDICATOR SWUNG VIOLENTLY. ABORTED TAKEOFF AND SECURED NR 2 ENGINE WITH APPROPRIATE CHECKLIST. REMOVED AND REPLACED NR 2 SURGE BLEED VALVE ON ENGINE NR 2 IN ACCORDANCE WITH DC-8 M/M 75-30-3; OPERATIONAL CHECK PERFORMED BY CREW WITNESS, OPERATIONAL CHECK ENGINE RUN ALL PARAMETERS FOUND WITHIN LIMITS IN ACCORDANCE WITH M/M 71-00.