As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CLIMB OUT WITH N1 AROUND 91%. LOUD BANG HEARD FROM ENGINE #1 FOLLOWED QUICKLY BY ENGINE SHUTDOWN. PERFORMED GVI OF #1 ENGINE. FOUND METAL FOD IN FIRST STAGE COMPRESSOR SECTION, WITH DAMAGE TO MULTIPLE INLET GUIDE VANES. NO OBVIOUS DAMAGE OR BIRD STRIKE OCCURRENCE TO WING OR FUSELAGE... ENGINE CHANGE IN PROGRESS