As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#2 ENGINE PRIMARY EXHAUST NOZZLE PERFORATED FACE SHEET HAS A CRACK IN ZONE 2 AT THE 6:00 POSITION MEASURING 1 INCH IN LENGTH; 13 INCHES FWD OF THE AFT WELD LINE. / [01] REMOVED AND REPLACED #2 ENGINE PRIMARY EXHAUST NOZZLE IAW AMM 78-11-01.