As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GEN AMPS INDICATIONS WERE 25-35 OFF OF EACH OTHER. #1 INDICATED 10-15 AMPS, #2 INDICATED 30-40 AMPS. AFTER AVIONICS CYCLED PITOT HEAT ON AND OFF, THE AMPS BEGAN FLUCTUATING 10-20 AMPS EACH. DURING SHUTDOWN AT IDLE THE AMPS INDICATED ONLY 5 AMPS DIFFERENCE. REMOVED AND REPLACED #1 CURRENT SENSOR IAW AMM 24-30-00, 4-6. T/F MOC COMPLETED GOOD.