As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND ON WALK AROUND A 3.5 INCH CRACK ON NR 2 ENGINE RIGHT CORE COWLING OUTER SKIN. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4471A052 WITH FAA 8110-3 DATED 16 APR 2010. DVI TO BE PERFORMED EVERY 3 FLIGHT CYCLES WITH PERMANENT REPAIR AT NEXT A-CHECK.