As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TAKEOFF, NR 2 ENGINE PNEUMATIC MANIFOLD FAILURE LIGHT CAME ON. DURING TAKEOFF THE EGT ON NR 2 ENGINE WAS HIGH 925 WITH N1 REDUCED TO 100 PERCENT INDICATING A PNEUMATIC LEAK. *S/D* THE NUMBER 2 ENGINE BLEED DUCT CLAMP FAILED. THE DUCT BROKE LOOSE CAUSING THE MANIFOLD FAILURE LIGHT TO ILLUMINATE. REPLACED CLAMPS AND DUCT, REPAIRED DAMAGE TO SURROUNDING AREA.