As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REJECTED T/O DUE TO NR 2 ENGINE LOOP B FAULT AT 20KTS. NR 2 LOOP B INOP, VERIFY AND RECORD IN AML/EAML THAT REMAINING LOOP OPERATES NORMALLY PRIOR TO EACH FLIGHT. R & R NR 2 ENG "B" FIRE LOOP UPPER CORE WIRE HARNESS IN REF TO A300-600 AMM 71-52-01-4.