What was found
NR 2 ENGINE EGT 936 DEGREES DURING CLIMB. FUEL FLOW 600 LBS HIGHER THAN THE NR 1 ENGINE. THE NR 2 ENGINE DID NOT EXCEED EGT LIMITS IAW AMM 72-00-00-991-59300-03-A. PERFORMED A VISUAL INSPECTION IAW EA AC-72R-33937, STEPS 1, 2, & 3. AIRCRAFT RETURNED TO SERVICE.