What was found
DURING PREFLIGHT INSPECTION, FOUND THE NR 1 ENGINE, FOUND THE ENGINE & WING CONTROL CIRCUIT BREAKER OPEN. ACFT GROUNDED IAW SSM 30-11-11. NR 2 ENGINE GROUND WING THERMAL ANTI-ICE SOLENOID RESISTANCE READS HIGH AT P5-11 CONNECTOR D648 PIN 29. DISCONNECTED THE CONNECTOR AND FOUND THE SOLENOID CONNECTOR CONTAMINATED. REMOVED AND REPLACED THE SOLENOID VALVE IAW AMM 30-11-12-400-801, STEPS 3A THROUGH 3H(S). OPS CHECKED NORMAL. GROUND VERIFICATION GOOD.