As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUEL LEAKING PAST MIXTURE CONTROL SHAFT SEALS. ACFT AND ENGINE HAS A TURBO NORMALIZING SYS INSTALLED. WHEN ELECTRIC FUEL PUMP OPERATED ON BOOST (LOW), ENGINE DRIVEN FUEL PUMP HAD A LEAKAGE RATE OF FUEL OF ABOUT 1 DRIP EVERY 1.5 TO 2 SECONDS.