The invention belongs to the field of aircraft structure design, and in particular relates to a retractable device for a door-ladder integrated cabin door. At present, the door-ladder integrated type cabin door structure is generally adopted on modern small passenger planes and helicopters. The existing door-ladder integrated type cabin door retractable device includes a hydraulic retractable device, an electric retractable device and a gas spring auxiliary retractable device. In order to adapt to modern aircraft design concepts, the retractable device of the door-ladder integrated hatch of the present invention adopts a wire rope assembly, and the cable drum assembly (4) of the wire rope assembly (2) is driven through a gear set and has a buffer structure. No need for on-board energy, low maintenance and operation costs, convenient and simple operation, stable performance, high reliability, no pollution, no noise, simple structure, long life, low cost, etc. It is the first choice of one-type hatch door retractable device, which has great economic application value.