As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLIMBING THROUGH 9000FT THE NR 2 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AND A 20 PSI SPLIT IN THE PRESSURE MANIFOLD. PERFORMED THE PROCEDURES, THE LIGHT EXTINGUISHED. OPERATED THE REMAINDER OF THE FLIGHT ON NR 2 BLEED. MAINTENANCE FOUND THE NR 3 ENGINE BLEED SHUTOFF DUCT CRACKED AT THE FLANGE. THE DUCT WAS REPLACED AND LEAK CHECKED IAW THE AMM.