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EFIS / Glass Cockpit (PFD, MFD)

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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.
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