INTEGRATED FLT. DIRECTOR SYSTEM
The system which computes, interrogates, and continuously displays basic attitude, position, and steering information in order to maintain a particular course, heading, or attitude. Does not include flight management system components, which should be assigned to JASC code 3460. Typical parts are integrated flight annunciator, integrated flight comparator, integrated flight computer/amplifier, integrated flight control and integrated flight indicators (i.e., horizontal situation indicator (HSI), attitude and direction indicator (ADI), attitude direction unit (ADU), heading and direction indicator (HDI), radio direction indicator (RDI), course direction indicator (CDI), flight director indicator (FDI), pictorial navigation indicator, flight command indicator, steering computer utilized in the integrated flight instrument systems, and other components such as cables, connectors, etc.