What was found
DURING CLIMB FROM KTOL NR 1 ENGINE ANTI-ICE LIGHT ILLUMINATED, OIL PRESSURE LIGHT FLICKERED, EGT DROPED TO 270°C, LOW PRESSURE PNEUMATIC CONTROL CIRCUIT BREAKER POPPED, ENGINE GENERATOR FAIL LIGHT ILLUMINATED WHILE VOLTS AND FREQUENIES WERE NORMAL. CLIMB POWER WAS SET AT EPR 1.70, AND EGT 560°C. THE ENGINE POWER LEVER WAS RETARDED TO IDLE AND ALL INDICATIONS RETURNED TO NORMAL. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE CENTER INTERMEDIATE ANTI-ICING AIR MANIFOLD FORWARD CLAMP BOLT BROKEN. MAINTENANCE REPLACED THE BOLT AND REPAIRED WIRES IN THE PYLON IAW DACO DC8 MM 20-50-1. THE OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.