As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE NR 2 OVERHEAT ON TAKEOFF, TOGA POWER USED. TEMPERATURE WENT BACK TO NORMAL EGT AFTER CLIMB POWER SELECTED. THE HIGH PRESSURE BLEED COUPLING HAD COME OFF AND WAS FOUND LYING IN THE THRUST REVERSER COMPARTMENT. THE THRUST REVERSER EXPERIENCED DAMAGE AS A RESULT OF FAILED DUCT CLAMP. R & R NR 2 ENGINE.