As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING ROUTINE FUEL NOZZLE CLEANING AND FLOW TEST IT WAS NOTICED THAT ONE FUEL NOZZLE SHEATH WAS CRACKED FROM THE AIR BLEED SLOT AT A 45 DEGREE ANGLE TOWARDS THE NOZZLE HOLE. THE SHEATH HAD 400 HOURS TIME IN SERVICE SINCE LAST INSPECTION. (TC NR 20070202009)