As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CREW NOTICED ENGINE NUMBER TWO N1 WAS 87.7% AND ENGINE NUMBER ONE N1 WAS 95% DURING TAKEOFF ROLL. AIRCRAFT WAS UNABLE TO CREATE ENOUGH POWER ON NR 2 FOR CONTINUED SAFE FLIGHT. FUEL PUMP PACK REPLACED. IAW AMM 73-11-01-400-801-F00.