What was found
DURING TAXIING, AS FLIGHT TAI-311, THE PILOT REPORTED STEERING FAILURE, SO THE ACFT WAS RETURNED TO THE GATE. IAW FIM 32-53-00-810-817-A, THE STEERING FEEDBACK SENSORS WERE ADJUSTED & FUNCTIONAL TEST PERFORMED IAW AMM 32-53-09 500 WITH NO EICAS FAILURE MSGS. THE ACFT WAS RETURNED TO SERVICE AFTER THE DESCRIBED MX ACTION.