What was found
AFTER TAKEOFF, SLAT FAIL EICAS MESSAGE WAS INDICATED FOLLOWED BY SHAKER ANTICIPATED AND AOA LIMIT FAIL. REPLACED LT SLAT 2/3 SKEW SENSOR DUE TO LOW INSULATION RESISTANCE, LESS THAN .01 MILLIOHMS TO GND, IAW AMM 27-83-01-401. THE AIRCRAFT WAS GROUNDED.