What was found
(CAN) UPON REACHING TOP OF CLIMB A SLAT FAIL EICAS CAUTION WAS GENERATED. FLIGHT CONTINUED AND LANDED IN A SLAT 0, FLAP 2, CONFIGURATION. REPLACED LT OTBD SLAT SKEW SENSOR .7500 AND RT OTBD SLAT SKEW SENSOR IAW AMM 27-83-01. ALSO REPLACED RT OTBD SLAT SKEW SENSOR HARNESS, W612 IAW AMM 27-83-07. SLAT/FLAP SYS OPS CHECK SERVICABLE.