What was found
AIRCRAFT AIR TURN BACK DUE TO ENGINE 2 FAILURE DURING INITIAL CLIMB, REACHING 660 DEGREE C OF EGT EMERGENCY PROCEDURE WAS PERFORMED. DURING REVISION THE EXHAUST CONE, SUPPRESSOR AND TURBINE FAN WITH DAMAGE. ENGINE NR 2 WAS REPLACED IAW MM, OPERATIONAL TEST WAS ACCOMPLISHED IAW MPCM, ALL CORRECT.