🔵✈️ 157. Most important features of Electronic Flight Instrument System (EFIS) in an airplane 🚁
Source: FAA-H-8083-31A, Aviation Maintenance Technician Handbook– Airframe, Volume 2, Pag: 10-70
Electronic Flight Instrument System (EFIS)
The flight instruments were the first to adopt computer technology and utilize flat screen, multifunctional displays (MFD). EFIS uses dedicated signal generators to drive two independent displays in the center of the basic T.
The attitude indicator and directional gyro are replaced by cathode ray tubes (CRT) used to display EADI and EHSI presentations. These enhanced instruments operate alongside ordinary mechanic and electric instruments with limited integration.
Still, EADI and EHSI technology is very desirable, reducing workload and panel scan with the added safety provided by integration of navigation information as described.
Early EFIS systems have analog technology, while newer models may be digital systems. The signal generators receive information from attitude and navigation equipment.
Through a display controller, the pilot can select the various mode or screen features wishing to be displayed. Independent dedicated pilot and copilot systems are normal. A third, backup symbol generator is available to assume operation should one of the two primary units fail.
Electronic depiction of ADI and HSI information is the core purpose of an EFIS system. Its expanded size and capabilities over traditional gauges allow for integration of even more flight instrument data. A vertical airspeed scale is typically displayed just left of the attitude field.
This is in the same relative position as the airspeed indicator in an analog basic T instrument panel. To the right of the attitude field, many EFIS systems display an altitude and vertical speed scale. Since most EFIS EADI depictions include the inclinometer, normally part of the turn coordinator, all of the basic flight instruments are depicted by the EFIS display.
| Type of Technology / System Component | Display Type | Integrated Instruments | Key Functions | Safety and Redundancy Features |
Electronic Attitude Director Indicator (EADI) Analog (early) or Digital (newer) | Cathode Ray Tube (CRT) or Flat Screen MFD | Attitude indicator, Airspeed indicator (vertical scale), Inclinometer, Altitude and Vertical speed scales | Electronic depiction of ADI information; replaces the attitude indicator in the basic T | Reduces pilot workload and panel scan; integrates navigation information |
Electronic Horizontal Situation Indicator (EHSI) Analog (early) or Digital (newer) | Cathode Ray Tube (CRT) or Flat Screen MFD | Directional gyro, Navigation information | Electronic depiction of HSI information; replaces the directional gyro in the basic T | Reduces workload and provides added safety via integration of navigation information |
Signal Generator Analog or Digital | Drives the independent displays; receives information from attitude and navigation equipment | A third, backup symbol generator is available to assume operation should one of the two primary units fail | ||
Display Controller | Allows the pilot to select various modes or screen features wishing to be displayed | Allows for independent pilot and copilot system configurations |