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In the 1990s, several commercial aviation firms and international aviation safety agencies began expanding CRM into air traffic control, aircraft design, and aircraft maintenance. The aircraft maintenance section of this training expansion gained traction as maintenance resource management (MRM).
ARINC 661 is a standard which aims to normalize the definition of a Cockpit Display System (CDS), and the communication between the CDS and User Applications (UA) which manage aircraft avionics functions. The GUI definition is completely defined in binary Definition Files (DF). [1]
ARINC 702A, Advanced Flight Management Computer System; Avionics, Element, Software and Functions Ch 20, Cary R. Spitzer, ISBN 0-8493-8438-9; FMC User's Guide B737, Ch 1, Bill Bulfer, Leading Edge Libraries; Casner, S.M. The Pilot's Guide to the Modern Airline Cockpit. Newcastle WA, Aviation Supplies and Academics, 2007. ISBN 1-56027-683-5.
The Airbus A320 family was the first airliner to feature a full glass cockpit and digital fly-by-wire flight control system. The only analogue instruments were the radio magnetic indicator, brake pressure indicator, standby altimeter and artificial horizon, the latter two being replaced by a digital integrated standby instrument system in later production models.
Improvements in computer technology, the need for enhancement of situational awareness in more complex environments, and the rapid growth of commercial air transportation, together with continued military competitiveness, led to increased levels of integration in the cockpit. The average transport aircraft in the mid-1970s had more than one ...
Electronic flight bag showing the airport diagram of Avalon Airport. An electronic flight bag (EFB) is an electronic information management device that helps flight crews perform flight management tasks more easily and efficiently with less paper [1] providing the reference material often found in the pilot's carry-on flight bag, including the flight-crew operating manual, navigational charts ...
Abstract representation of a Fly-By-Wire flight system. A flight control computer (FCC) is a primary component of the avionics system found in fly-by-wire aircraft. It is a specialized computer system that can create artificial flight characteristics and improve handling characteristics by automating a variety of in-flight tasks which reduce the workload on the cockpit flight crew.
FAA FITS compliant training is recommended for any pilot transitioning to the G1000 or any other glass cockpit prior to operating the aircraft in instrument meteorological conditions (IMC) or if operating a glass cockpit aircraft for the first time. Glass cockpit aircraft may not be suitable for primary training. [7] One of the most effective ...