What was found
SIMULTANEOUS DUAL FMC FAILURE DURING CRUISE, ROLL MODE WENT TO CWS WITH ALTITUDE HOLD DISPLAYED, RETURNED TO NORMAL AFTER APPROX 10-15 SECONDS, REENGAGED CNAV/VNAV. ACFT GROUNDED. HARDWARE FAULTS, SENSOR STATUS & IN FLIGHT FAULTS LEG 1 SHOWS NO FAULTS. SYS GROUND VERIFICATION CHECKED GOOD. ACCOMPLISHED FIM 34-61, TASK 801 & 837 TO RT FMC FOUND NO SOFTWARE OR HARWARE FAULTS. SENSOR STATUS & IN FLIGHT FAULTS LEG 1 SHOWS NO FAULTS. SYSTEM GROUND VERIFICATION CHECKED GOOD.