As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.