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  2. Garmin G1000 - Wikipedia

    en.wikipedia.org/wiki/Garmin_G1000

    Garmin announced its first G1000 retrofit program for the Beechcraft C90 King Air in 2007. That same year the Garmin G1000 became a jet platform, as the avionics system for the Cessna Citation Mustang very light jet. Versions of the G1000 are also used in the Embraer Phenom 100 and Embraer Phenom 300, and PiperJet, as well as the Bell SLS ...

  3. Primary flight display - Wikipedia

    en.wikipedia.org/wiki/Primary_flight_display

    PFD with key instrument displays labelled PFD of a Garmin G1000. The details of the display layout on a primary flight display can vary enormously, depending on the aircraft, the aircraft's manufacturer, the specific model of PFD, certain settings chosen by the pilot, and various internal options that are selected by the aircraft's owner (i.e., an airline, in the case of a large airliner).

  4. Electronic flight instrument system - Wikipedia

    en.wikipedia.org/wiki/Electronic_flight...

    In aviation, an electronic flight instrument system (EFIS) is a flight instrument display system in an aircraft cockpit that displays flight data electronically rather than electromechanically. An EFIS normally consists of a primary flight display (PFD), multi-function display (MFD), and an engine indicating and crew alerting system (EICAS ...

  5. Horizontal situation indicator - Wikipedia

    en.wikipedia.org/wiki/Horizontal_situation_indicator

    The HSI can reduce pilot workload by lessening the number of elements in the pilot's instrument scan to the six basic flight instruments. Among other advantages, the HSI offers freedom from the confusion of reverse sensing on an instrument landing system localizer back course approach. As long as the needle is set to the localizer front course ...

  6. Attitude and heading reference system - Wikipedia

    en.wikipedia.org/wiki/Attitude_and_heading...

    An attitude and heading reference system (AHRS) consists of sensors on three axes that provide attitude information for aircraft, including roll, pitch, and yaw.These are sometimes referred to as MARG (Magnetic, Angular Rate, and Gravity) [1] sensors and consist of either solid-state or microelectromechanical systems (MEMS) gyroscopes, accelerometers and magnetometers.

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