The invention belongs to the technical field of aviation and relates to an overturning plate type electric control valve device. The device comprises an upper shell, a lower shell, a first oil way anda second oil way, wherein the first oil way and the second oil way are arranged between the upper shell and the lower shell. The first oil way and the second oil way common use the same inlet and thesame outlet. An electromagnetic valve is arranged on the first oil way, and a piston is arranged at the position, between the inlet and the electromagnetic valve, on the first oil way. A valve is arranged on the second oil way. When the electromagnetic valve is electrified, the first oil way is cut off, the piston abuts against the valve, the valve is forced to be closed, and the second oil way is cut off; and when the electromagnetic valve is not electrified, the first oil way is smooth, oil liquid entering the second oil way pushes the valve under the effect of the oil liquid, and thereforethe second oil way can be smooth.