What was found
WHILE ACCOMPLISHING T/C 78472000 #2 ENGINE FOUND FAN INLET CASE DAMAGE APPROX. 8 INCHES FWD OF O/B ENGINE CRADLE MOUNT AREA. 700X .150. GROUNDED - YES. REMOVED HIGH METAL AND SWAP ETCHED AREA PER B737-800 AMM 72-23-05-700 2.F.(1) & (2). FOUND GOUGE TO BE .004 DEEP WITHIN LIMITS EBM 72-23-31. ACCOMPLISHED FPI AMM 70-40-01/201 NO RELEVANT INDICATIONS AFTER BLEND OUT. APPLIED OXIDE FILM COATING TO SUBJECT AREA PER AMM 72-23-05-700-SUBTASK 72-23-05-390-001-F00(5).