As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING RUN-UP, GEN AMP DIFFERENCE GREATER THAN 10 AMPS. AT ONE POINT THE #1 GEN HAD +5 AMP WHILE THE #2 GEN HAD +40 AMP. REMOVED AND REPLACED #1 GENERATOR CURRENT TRANSFORMER IAW AMM 24-30-00, 4-6. T/F MOC COMPLETED IAW MSM 05-60-00, 6-12.