What is EFIS / Glass Cockpit?
EFIS (Electronic Flight Instrument System) is an integrated cockpit display system that replaces classical round mechanical instruments ("steam gauges") with digital, computer-driven displays. "Glass cockpit" is the colloquial term for a cockpit with predominantly EFIS displays.
Advantages over mechanical instruments:
- Clearer presentation,
- Integration of multiple data on one screen,
- Programmable/configurable (layout, units, symbology),
- Lower weight and fewer moving parts,
- Better diagnostics and self-tests.
Disadvantages:
- Full dependence on the electrical system and computer,
- Requires pilot training (Differences Training under FCL.710),
- On failure: fallback to standby instruments is mandatory.
Main EFIS components
Primary Flight Display (PFD)
The PFD replaces the classical "Six Pack" flight instruments (airspeed, attitude, altitude, turn, heading, VSI). Typical elements:
- Attitude indicator as the central element, often filling the entire screen width.
- Airspeed tape (vertical speed band) on the left: current speed as digits, V-speeds (Vs0, Vs, Vfe, Vno, Vne) as coloured markings, trend vector.
- Altitude tape on the right: current altitude as digits, selected altitude (FMS/bug), QNH display.
- Vertical Speed Indicator (VSI) beside altitude tape, as scale or digit.
- Heading indicator (HSI) below: compass-style, with selected heading bug, CDI deviation (VOR/GPS), DME, ETA.
- Slip/skid indicator as a trapezoid below the attitude display.
- Trend/bug indicators: selected altitude, heading, airspeed, V-speeds.
Multi-Function Display (MFD)
The MFD shows non-primary information:
- Moving map with chart, flight path, waypoints, airspace,
- Engine indications (engine monitoring): MAP, RPM, EGT, CHT, oil pressure/temperature, fuel,
- Flight plan and navigation,
- TAWS / terrain awareness with terrain warnings,
- Weather radar / stormscope / datalink weather,
- Traffic information (TIS, ADS-B IN),
- Checklists, approach charts.
Common GA glass-cockpit platforms
- Garmin G1000 / G1000 NXi — widespread (C172, C182, DA40, DA42, …).
- Garmin G3X Touch — Experimental and now certified.
- Dynon SkyView / HDX — Experimental and certified types (STC).
- Avidyne Entegra.
- Aspen Evolution — retrofit PFD for standard 3" instrument hole.
Display technologies
LCD (Liquid Crystal Display) — current standard:
- Backlit, high resolution, low power consumption.
- TFT active-matrix LCDs with wide viewing angle.
OLED and AMOLED — rare on certified aircraft due to lifetime and temperature requirements.
Limitations:
- Direct-sun reflections — sun-shade, polarising filters, high brightness (1 000+ cd/m²).
- Temperature range — typically −20 °C to +55 °C; cold start may delay boot.
- Boot-up time — a few seconds to one minute.
Symbology
EFIS symbology follows ARINC 661 and DO-178C as software certification standards. Typical symbols:
- Attitude: blue sky above, brown ground below, white horizon with pitch scales, bank pointer at top with markings at 10°, 20°, 30°, 45°, 60°.
- Speed tape: white = Vs0–Vs1, green = Vs–Vno, yellow = Vno–Vne, red line = Vne.
- Altitude tape: large digits for thousands, smaller for hundreds; selected altitude as bug.
- HSI: red lubber line forward, rotating compass card, CDI display.
Failover / standby instruments
EASA and FAA require for IFR-certified glass-cockpit aircraft:
- Standby attitude indicator (mechanical or self-battery),
- Standby airspeed indicator,
- Standby altimeter,
- Standby compass (magnetic "whiskey" compass).
On PFD failure the pilot switches to standby instruments — should be trained routinely.
Reversionary mode
On failure of one display the other can take over — the so-called reversionary mode: PFD and MFD functions are consolidated on a single screen (smaller fonts, congested). In G1000: red "RVRT" knob or automatic on fault detection.
Pilot requirements
Differences Training under Regulation (EU) 1178/2011 FCL.710 is required when a pilot moves from analogue instruments to glass cockpit. Content:
- Operation of knob/touchscreen concepts,
- Symbology and layout,
- Reversionary mode and standby procedures,
- GPS navigation, flight plan, direct-to.