As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON WALK AROUND FOUND DAMAGE TO NR 4 ENGINE RIGHT CORE COWLING OUTER SKIN AT FORWARD EDGE 6 O'CLOCK POSITION. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A054 WITH FAA 8110-3 DATED 18 APR 2010 TO TRIM DAMAGE AND APPLY SPEED TAPE. DVI TO BE PERFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHECK.