As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON DEPARTURE, NR 2 ENGINE REACHED TEMP LIMITS PRIR TO REACHING T/O. THRUST WAS REDUCED TO 1.85 EPR TO MAINTAIN TEMP LIMITS. ALL OTHER ENGINE INDICATION SHOWED NORMAL. ON CLIMBOUT TEMP STAYED AT MAX, WITH CHARTED CLIMB THRUST. COULD NOT DUPLICATED, SWAPPED NR 2 AND NR 3 INDICATORS FOR TROUBLESHOOTING. RAN AT TAKEOFF POWER FOR 3 MINUTES, MAX EGT WAS 565 DEGREES.