Integrated Instruments – Electronic Displays
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Topics in this section
- 022-13-01Electronic Display Units in EFIS: Redundancy, Switching, and Priority Logic
Study EFIS display-unit architecture, automatic reconfiguration after DU failures, and information-priority logic that preserves critical flight displays.
- 022-13-03Electronic Flight Instrument Systems (EFIS): PFD/ND Modes and Standby Logic
Learn EFIS architecture, PFD and ND presentation modes, control-panel overlays, and ISIS standby operation in case of primary display failure.
- 022-13-04EICAS and ECAM: Engine Parameters, Alerts, and Electronic Checklists
Understand EICAS/ECAM display philosophy, alerting integration, and checklist limitations that require informed crew judgment and CRM discipline.
- 022-13-06Electronic Flight Bag (EFB): Classes, Functions, and Operational Risks
Study EFB functionality, hardware/software classes, certification boundaries, and operational error paths such as incorrect performance-data entry.
- 022-13-07HUD, EVS, and SVS: Vision Technologies, Minima, and Limitations
Compare HUD, EVS, and SVS capabilities in modern cockpits, including visibility benefits, operational minima effects, and data-source limitations.