As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 BLEED FAULT DURING CLIMB-OUT. FAULT DUE TO OVERHEAT. PRESSURED CHECKED MUSCLE LINE ON FAN AIR VALVE TO HP VALVE. CHECKED GOOD. REPLACED FAN AIR VALVE IAW MM 36-11-16-4-02. RAN NR 2 ENGINE AT POWER PER JRH. WITH ENGINE STABILIZED AT POWER THE BLEED PRESSURE WAS 42 PSI AND DUCT TEMP WAS 180C. NO OVERHEAT FAULTS, ALL INDICATIONS NORMAL.