As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEUDLED INSPECTION, THE NR 1 COMBUSTION CAN ASSY ON THE LEFT ENGINE WAS REJECTED DUE TO AN OUTER CASING BURN-THROUGH NEAR THE AFT END. UPON CAN REMOVAL, THE FLAME TUBE WAS FOUND CRACKED 360 DEGREES AND SEPARATED APPROXIMATELY 4 INCHES - 5 INCHES FROM THE AFT END. NO DOWN STREAM IMPACT OR TEMPERATURE DISTRESS NOTED. THE DAMAGED PARTS WILL BE REPLACED. THE COMBUSTION CAN WILL BE SENT TO RR.