What was found
GE DIAGNOSTICS REPORTS THE #1 ENGINE EXPERIENCED AN EGT EXCEEDANCE DURING TAKEOFF THAT MAY HAVE EXCEEDED THE TRANSIENT AREA LIMITS. PEAK EGT RECORDED ON REPORT 06 WAS 966 DEGREES DURING TAKEOFF (FLIGHT PHASE 4) GROUNDED - YES. PERFORMED GVI OF #1 ENGINE INLET AND EXHAUST, NO DEFECTS NOTED REF B737-800 AMM 71-00-00-800-804-F00. EEC BITE CHECK SHOWED AN EXCEEDANCE PEAK 967.0 AND IN THE RED SHOWED FOR 7.6 SECONDS (AREA B) NO ENGINE FAULTS RECORDED DURING ACCOMPLISHMENT OF FMC/CDU ENGINE BITE CHECK. REF LP 60345395 FOR PLT DEFERRAL TO TROUBLESHOOT AND, IF POSSIBLE CORRECT THE CAUSE OF THE EGT OVERTEMPERATURE.