As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF ROLL, RIGHT ENGINE ITT ABOVE 765 DEGREES. DURING GROUND OPERATION WITH BLEEDS ON THERE IS A 50 DEGREES DIFFERENCE. REMOVED AND REPLACED RT ENGINE DIFFUSER TUBE AT 10 O`CLOCK POSITION IAW MM 72-30-00. PERFORMED RUNUP IAW JIC 72-00-00. ALL PARAMETERS WITHIN LIMITS AT THIS TIME.