Method and system for autoflight information display

A method and system for autoflight information display. A method in accordance with one embodiment of the invention includes determining if an automatic aircraft controller is controlling an aircraft function based at least in part on a target aircraft speed. If so, the method further includes displaying alphanumeric information corresponding to the operation of the automatic aircraft controller at a first location of a display medium. If not, the method further includes displaying the alphanumeric information at a second location of the display medium different than the first location. The first location can be aligned with a display of the aircraft speed, and the second location can be aligned with a display of the aircraft altitude. In another embodiment of the invention, engine control information can be integrated with a display of aircraft autopilot and/or autothrottle information.