What was found
AIR TURNBACK. FLIGHT CREW REPORTED NR 1 ENGINE ANTI-ICE VALVES INDICATED OPEN ON OVERHEAD PANEL. AT CLIMB POWER, NR 1 ENGINE EPR AT APPROXIMATELY 87 PERCENT AND NR 2 ENGINE EPR AT 90 PERCENT. REPLACED NR 1 ENGINE EPR TRANSMITTER PER MM 77-11-21. PERFORMED ENGINE RUN PER MM 71-09-236, PAGE 206, AND FOUND TO BE WITHIN LIMITS.