As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING WALK AROUND CHECK, MX FOUND 2EA CRACKS AT 7 O'CLOCK POSITION ON THE AFT CENTER BODY ON THE NR 2 ENGINE. 1EA CRACK MEASURING 1.25 INCHES AND 1EA CRACK MEASURING APPROX 1 INCH REF FIGURE 1. DISPOSITION WAS MADE TO STOP DRILL THE CRACKS USING STANDARD PRACTICES AND ELEMENTARY OPERATIONS; RE-INSPECT EVERY FLIGHT CYCLE; AND REPLACE CENTERBODY WITHIN 10 FLIGHT CYCLES. THIS EO IS APPROVED BY 8110-3 DATED JULY 31, 2011.