As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS SIGNIFICANT SYS - NR 2 ENGINE 1 FAN BLADE BENT ON L/E .3750" FROM TIP, 2" LONG. BEND IS .1250" IN DEFLECTION AFT. R & R NR 5 AND 24 FAN BLADE IAW AMM 72-31-02-004-001 N00. PERFORMED TEST 8 VIBRATION SURVEY IAW AMM 71-00-00-725-008-N00. NO TROUBLE FOUND ON SURVEY ACFT OK FOR SVC.