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Avionics displays

 

 

EFIS and Pilot/Flight Deck Interfaces

 

The layout, controls, displays and amount of automation in flight decks have evolved tremendously in commercial aviation. What is sometimes termed the "classic" flight deck, which includes the B-727, the DC-10, and early series B-747, is typically characterized by dedicated flight displays, where one piece of data is generally shown on a dedicated gauge or dial as the form of display. These aircraft are relatively lacking in automation. All of these aircraft are further characterized by the relative simplicity of their autopilot, which offers one or a few simple modes in each axis. In general, a single instrument indicates the parameter of a single sensor. In a few cases, such as the Horizontal Situation Indicator, a single instrument indicates the "raw" output of multiple sensors. Regardless, the crew is generally responsible for monitoring the various instruments and realizing when a parameter is out of range. A simple caution and warning system exists, but it covers only the most critical system failures.

 

The first generation of "glass cockpit" flight decks, which include the B-757/767, A-310, and MD-88, receive their nickname due to their use of cathode ray tubes (CRTs). A mix of CRTs and instruments was used in this generation of flight deck, with instruments used for primary flight information such as airspeed and altitude. EFIS installations have the following components:

displays, controls and data processors. A key innovation in these flight decks was the "map display" and its coupling to the Flight Management Systems (FMS). This enabled the crew to program their flight plan into a computer and see their planned track along the ground, with associated waypoints, on the map display. Accompanying the introduction of the map display and FMS were more complex autopilots (added modes from the FMS and other requirements). This generation of aircraft also featured the introduction of an integrated Caution and Warning System, usually displayed in a centre CRT with engine information. A major feature of this Caution and Warning System was that it prioritized alerts according a strict hierarchy of "warnings" (immediate crew action required), "cautions" (immediate crew awareness and future action required), and "advisories" (crew awareness and possible action required)."

 

 

Electronic flight instrument systems

 

The second generation of "glass cockpit" flight decks, which include the B-747-400, A-320/330/340, F70/100, MD-11, and B-777, are characterized by the prevalence of CRTs (or LCDs in the case of the B-777) on the primary instrument panel. CRT/LCDs are used for all primary flight information, which is integrated on a few displays. In this generation of flight deck, there is some integration of the FMS and autopilot - certain pilot commands can be input into either the FMS or autopilot and automatically routed to the other.

 

 

Primary Flight Displays PFDs and secondary flight displays SFDS

 

There are varying levels of aircraft systems automation in this generation of flight deck. For example, the MD-11 fuel system can suffer certain failures and take corrective action - the crew is only notified if they must take some action or if the failure affects aircraft performance. The caution and warning systems in this generation of flight decks are sometimes accompanied by synoptic displays that graphically indicate problems. Some of these flight decks feature fly-by-wire control systems - in the case of the A320/330/340, this capability has allowed the manufacturer to tailor the control laws such that the flying qualities of these various size aircraft appear similar to pilots. The latest addition to this generation of flight decks, the B-777, has incorporated "cursor control" for certain displays, allowing the flight crew to use a touchpad to interact with "soft buttons" programmed on these flight displays.

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