What was found
DURING TAKEOFF AT 1,500 FT, RIGHT ENGINE EXCEEDED ITT RED LINE PRIOR TO FLAP RETRACT ALTITUDE. COMPLIED WITH EXTENSIVE TROUBLESHOOTING. REF MESA WORK ORDER REV. 45358 FOR >FULL DETAILS. REPLACED BLEED AIR SEALS AS NEEDED. COMPLETED A COMPRESSOR WASH AND BLADE CLEANING IAW MM 71-00-00. COMPLETED A CAPPED 5 POINT RUN AFTERWARDS. ENTERED IN THE DATA IN THE ENGINE CALIBRATION RUN DATA SHEET. THE RESULTS WERE FOUND TO BE AN ACCEPTABLE MARGIN FOR A FLIGHT TO A MANUFACTURER FACILITY FOR FURTHER MAINTENANCE. REMOVED THE BLANK OFF PLATES AND PUT IN NEW GASKETS, RAN THE ENGINE AND LEAK CHECKED GOOD. INSTALLED THE UPPER AND LOWER COWLING.