What was found
THE FLIGHT CREW REPORTED THAT ON CLIMBOUT THE EDS FAULT ANNUNCIATOR ILLUMINATED WITH THE RIGHT ENGINE ITT RED. EXCEEDANCE TO 805 DEGREES. THE FLIGHT CREW REDUCED THRUST TO KEEP ITT WITHIN LIMITS. THE FLIGHT CREW ALSO NOTED THAT AT 785 DEGREES, THE FUEL FLOW WAS 100 POUNDS PER HOUR HIGHER THEN THE LEFT ENGINE. THE MAINTENANCE VENDOR TROUBLESHOT AND FOUND FAULTS WITH THE INBOARD 2.8 COMPRESSOR BLEED VALVE AND THE OUTBOARD 2.5 COMPRESSOR BLEED VALVE DEFECTIVE. THE COMPRESSOR VALVES WERE REPLACED WITH OVERHAULED UNITS. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2.8 VALVE P/N 31B5756-01 S/N AHX013190 2.5 VALVE P/N 31B5759-01 S/N AHX103100