An actuation system to control first and second flight control members on a vehicle , the actuation system comprising: a first pair of hydraulic actuators that are operatively connected to a first flight control member ; a second pair of hydraulic actuators that are operatively connected to a second flight control member ; a hydraulic fluid line that extends between each hydraulic actuator of the first pair of hydraulic actuators and the second pair of hydraulic actuators , said hydraulic fluid line supplying and returning hydraulic fluid from a hydraulic system in the vehicle to the hydraulic actuators to either deploy or retract the flight control members ; a first synchronization member that extends between the first pair of hydraulic actuators to synchronize movements of the first pair of hydraulic actuators ; a second synchronization member that extends between the second pair of hydraulic actuators to synchronize movements of the second pair of hydraulic actuators , the second synchronization member being independent from the first synchronization member ; a first brake to prevent movement of the first synchronization member ; a second brake to prevent movement of the second synchronization member ; a first motor operatively connected to the first synchronization member to adjust the first pair of hydraulic actuators to adjust a position of the first flight control member independently from the second flight control member ; a second motor operatively connected to the second synchronization member to adjust the second pair of hydraulic actuators to adjust a position of the second flight control member independently from the first flight control member ; and wherein the first and second synchronization members are positioned within the hydraulic fluid line . a first pair of hydraulic actuators that are operatively connected to a first flight control member ; a second pair of hydraulic actuators that are operatively connected to a second flight control member ; a hydraulic fluid line that extends between each hydraulic actuator of the first pair of hydraulic actuators and the second pair of hydraulic actuators , said hydraulic fluid line supplying and returning hydraulic fluid from a hydraulic system in the vehicle to the hydraulic actuators to either deploy or retract the flight control members ; a first synchronization member that extends between the first pair of hydraulic actuators to synchronize movements of the first pair of hydraulic actuators ; a second synchronization member that extends between the second pair of hydraulic actuators to synchronize movements of the second pair of hydraulic actuators , the second synchronization member being independent from the first synchronization member ; a first brake to prevent movement of the first synchronization member ; a second brake to prevent movement of the second synchronization member ; a first motor operatively connected to the first synchronization member to adjust the first pair of hydraulic actuators to adjust a position of the first flight control member independently from the second flight control member ; a second motor operatively connected to the second synchronization member to adjust the second pair of hydraulic actuators to adjust a position of the second flight control member independently from the first flight control member ; and wherein the first and second synchronization members are positioned within the hydraulic fluid line . <EOS>