The airplane has a self-sufficient emergency release unit provided with a determination device that determines a sinking speed of the airplane. A control device triggers automatic landing during exceeding of preset sinking speed. A parachute is present at a shelf, and a camera is present below a nose of the airplane. A wing is fixed in the center of the airplane, and a drive is present in a rear of the airplane. An antenna is attached to a rear third of the airplane behind the wing. A threshold value of the sinking speed is input into the control device before starting of the airplane. An independent claim is also included for a method for rescuing an unmanned or manned airplane.
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