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.