The Anderson Greenwood AG-14 is a two-seat utility aircraft developed in the United States shortly after World War II.

It is an all-metal, shoulder-wing monoplane of pod-and-boom configuration, equipped with a pusher propeller, side-by-side seating and fixed tricycle undercarriage.

Eventually, only five more examples were built before Anderson Greenwood abandoned the project in favour of producing aircraft components for other manufacturers.

[1][2] Wind tunnel testing determined that a shoulder wing was ideal for minimal wing-body airflow separation that is intrinsic to a pusher configuration.

A four inch propeller shaft extension allows the engine to be mounted closer to the aircraft's center of gravity.

[7] In 1986 the Anderson Greenwood Company donated an AG-14, serial number 3, registered as N314AG to the Experimental Aircraft Association Aviation Foundation.