As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING NR 2 ENGINE START TOW CREW REPORTED FOD INGESTION. FOUND NR 2 ENGINE RUB STRIP DAMAGE. SCORED ROUND CIRCUMFERENCE OF RUBSTRIP 6 INCHES FROM FRONT EDGE MEASURING 1.5 INCHES FRONT- BACK 0.070 INCH DEEP. ACCOMPLISHED VISUAL INSP, NO OTHER DAMAGE FOUND. NR 2 ENGINE RUBSTRIP DAMAGE WITHIN LIMITS PER MM. CREW REPORTED NO ABNORMAL INDICATIONS DURING ENGINE START.