Ejectable door for aircraft

Aircraft door comprising a frame that can be fixed to the fuselage of the aircraft, a panel articulated onto the frame by articulation means, stops and mechanical elements installed on the panel and on the frame respectively, so as to remain in mutual contact under the effect of the weight of the panel when the door is closed, and guide means inserted between the panel and the frame in order to automatically release/engage the stops with respect to the mechanical elements, at the beginning of opening and at the end of closing of the door respectively, in which the said door also comprises ejection triggering means, that can control mechanical disconnection of the articulation means and a relative disengagement of the stops from the mechanical elements, the guide means enabling downwards displacement of the panel by gravity when the ejection triggering means are used.