As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING PHASE 1 THROUGH 4 INSPECTION, OBSERVED THE LEFT ENGINE STARTER/GENERTOR R.F. NOISE SUPPRESSION CAPACITOR UNIT HAD EVIDENCE OF EXTREME OVERHEAT. OUTER CASE DISTORTED AND DISCOLORED. TERMINAL ISOLATOR DISTORTED AND CHARRED. CONTINUED OPERATION COULD HAVE RESULTED IN AN IN-FLIGHT FIRE.