As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS SIGNIFICANT SYSTEM, RIGHT ENGINE HUNG START ON FIRST ATTEMPT, ENGINE REACHED 50 PERCENT N2 STARTER CUTOUT THEN N2 WOUND DOWN TO 46 PERCENT EGT INCREASING TO 440 DEGS C ABORTED START. RESTART SUCCESSFUL BUT ENGINE VERY SLOW TO STABLIZE. PRECAUTIONARY REMOVED AND REPLACED NR 2 FUEL PUMP FILTER PER AMM 73-11-02-404-019. LEAK CHECK OK PERFORMED GROUND IDLE RUN PER AMM 71-00-00-802. ALL INDICATIONS NORMAL NR 2 ENGINE STABLIZED AT 67% N2 WITHIN 90 SECONDS.