What was found
ON DESCENT WHILE CONFIGURING FOR THE APPROACH WITH FLAPS SELECTED TO LAND 1/2 SPEED BRAKES, RECEIVED THE FOLLOWING EICAS MSGS. SLAT FAIL, SPOILER FAULT, AOA LIMIT FAIL & SHAKE ANTICIPATED, AFTER REFERENCIN QRH, LANDED WITH FLAPS 2 & SLATS ZERO (0) CONFIGURATION. DUE TO NUMEROUS DIVERGING OF FLAPS/SLATS HANDLE INPUTS CREATED A LATCH FAULT IN THE SF-ACE 1 COMPUTER. PERFORMED ELECTRICAL RE-RIGGING OF SF-ACES COMPUTER IAW AMM 27-80-00-820-802-A, COULD NOT DUPLICATE FAULT. PERFORMED RETURN TO SERVICE TEST OF THE FLIGHT CONTROL SYSTEM IAW AMM 27-00-00-070-801-A/200. NO MESSAGE PRESENT. A/C OK FOR SERVICE.