What was found
ETOPS - #2 ENGINE BIRD STRIKE DAMAGE. NEED TO REMOVE ENG 2 FAN BLADES (1-20) DAMAGE OUT OF LIMITS. REMOVED FAN BLADES ON ENG 2 (1-20) PER AMM 72-11-01-000-801-A. REMOVED INLET CONE PER AMM 72-11-01-000-801-A. INSTALLED #2 ENGINE FAN BLADES #1-20 PER A321 TASK 72-11-03-400-801-A. INSTALLED #2 ENG INLET CONE PER A321 TASK 72-11-01-400-001. PERFORMED IDLE AND HIGH POWER ENGINE RUN. NO DEFECTS NOTED DURING ENGINE RUN. ENG VIB STAYED NORMAL. #2 ENG OK FOR SERVICE PER AMM 71-00-00.