As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MX WALK AROUND, FOUND A CRACK ON ENGINE NR 3 PRIMARY EXHAUST NOZZLE LOCATED AT 9 O'CLOCK POSITION AFT EDGE. THE CRACK DIMENSION RUNS 4.7500" LONG CIRCUMFERENTIAL AND LOCATED .7500" FROM THE NOZZLE AFT END. THE CRACK IS DETERMINED TO BE OUTSIDE ALLOWABLE LIMITS IAW SRM 54-41-30. DISPOSITION IS TO PERFORM TIME LIMITED REPAIR BY STOP DRILLING THE CRACK ENDS WITH A 0.125" DIAMETER HOLE, DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FC (FLIGHT CYCLES).