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Airbus A350 Warning Display ECAM on an Airbus A380 at the center ECAM on an Airbus A400M at the center. An electronic centralised aircraft monitoring (ECAM) or electronic centralized aircraft monitoring is a system that monitors aircraft functions and relays them to the pilots. It also produces messages detailing failures and in certain cases ...
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 ...
On some Bombardier aircraft, it is possible to call up the wrong checklist. Messages forbidding take-off can be shown as advisories. [3] The 757, 767, and 747-400 have no electronic checklists. The ERJ and the E-Jets have no electronic checklists. The CRJ have no electronic checklists. The Do-328 and the Do-328JET have no electronic checklists.
An annunciator panel, also known in some aircraft as the Centralized Warning Panel (CWP) or Caution Advisory Panel (CAP), is a group of lights used as a central indicator of status of equipment or systems in an aircraft, industrial process, building or other installation. Usually, the annunciator panel includes a main warning lamp or audible ...
ECAM may refer to: Electronic centralised aircraft monitor, a system that monitors aircraft functions and relays them to the pilots; Evidence-Based Complementary and Alternative Medicine, a medical journal; École Catholique des Arts et Métiers, an engineering school in Lyon, France; ECAM Rennes - Louis de Broglie, an engineering school in ...
Simplified glass cockpit of an Airbus A220, featuring unified LCD screens for both pilots to reduce pilot workload. A glass cockpit is an aircraft cockpit that features an array of electronic (digital) flight instrument displays, typically large LCD screens, rather than traditional analog dials and gauges. [1]
However, simple electronic hardware is within the scope of DO-254/ED-80 and applicants propose and use the guidance in this standard to obtain certification approval of simple custom micro-coded components, especially devices that support higher level (A/B) aircraft functions. [3] [4]
In aircraft in which the flight control system is fly-by-wire, the movements the pilot makes to the yoke or joystick in the cockpit, to control the flight, are converted to electronic signals, which are transmitted to the flight control computers that determine how to move each control surface to provide the aircraft movement the pilot ordered.