As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ONE ENGINE START, CREW NOTICED SLOW START ON NR 2 ENGINE AND 100 DEGREE CELCIUS EGT SPLIT DURING FLIGHT. UPON ARRIVAL AT DESTINATION, MAINTENANCE WAS NOTIFIED, INSPECTOR FOUND A 6 INCH CRACK ON COMBUSTOR CAN WHICH ALLOWED HOT BLEED AIR TO LEAK INTO ENGINE NACELLE CAUSING ENGINE POWER LOSS. ALSO, FOUND DENTS ON EXTERNAL SURFACE OF COMBUSTOR. ENGINE REPAIRED BY MANUFACTURER AND RETURNED TO SERVICE.