What was found
DURING CLIMBOUT, TURNED ON ENGINE ANTI-ICE, NO BLUE LIGHT INDICATION. CHECKED CIRCUIT BREAKER PANEL AND CB A-6, ENG 1, ENG WING CONTROL WAS TRIPPED. R & R NR 2 ENG MW0311 STRUT HARNESS REF AMM TASK 73-21-06-000-802-F00 AND TASK 73-21-06-400-802-F00. PERFORMED GROUND WING THERMAL ANTI-ICE TAI SOLENOID VALVE TEST OPS CK GOOD REF AMM TASK 30-11-12-710-801. PERFORMED AVM SYS OPERATIONALS G RUN. ACCOMPLISHED GROUND VERIFICATION CK NO FAULTS NOTED. C/B A-6 ENG WING CONTROL STAY IN OPS NORMAL.