An aircraft system may include a civil radio, a mission radio, and an adaptive flight display. The adaptive flight display may include a display, a processor, and memory. The memory may maintain a civil radio tuning system application and a mission radio tuning system application. The civil radio tuning system application and the mission radio tuning system application may be associated with the civil radio and the mission radio, respectively. The processor may be configured to: execute the civil radio tuning system application and the mission radio tuning system application; tune the civil and mission radios; generate a graphical user interface multifunction window including slots; assign slots to display information associated with the civil and mission radio tuning system applications; and output, to the display, the graphical user interface multifunction window having particular slots filled with the information associated with the civil and mission radio tuning system applications.