As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER T/O ALL INSTR PWR BY NR 2 ENG GEN SYS START SPIKING, LIGHT FLICKER. NR 2 FUEL FLOW IND AND NR 2 N2 FLUCT. FUEL PUMPS FAIL. A/C DIVERTED TO ATL. MX FOUND BURNED PIN ON NR 2 ENG GEN FEEDER HARNESS CONNECTOR VC4955P. REPLACED THE NR 2 GEN LINE. MX FOUND ECAM FREQ IND INOP.