As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
GENERATOR SPLIT GREATER THAN 10 AMPS. INDICATIONS WERE NORMAL AT IDLE, THEN ONCE AT FLY #1 GENERATOR SHOWED 10 AMPS WHILE #2 SHOWED 75 AMPS. AVIONICS RESET DID NOT RESOLVE ISSUE. WHILE TROUBLESHOOTING AIRCRAFT, DETECTED FLUCTUATION ON #1 ENGINE OF 5 AMPS TO 35 AMPS ON BOTH THE AMP METER ALONG WITH THE VEMD, WHILE #2 WAS STEADY AT 35 AMPS INDICATING THAT THE #1 CURRENT TRANSFORMER WAS BAD.