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ENGINE INDICATING AND CREW ALERTING SYSTEM ENGINE INDICATING AND CREW ALERTING SYSTEM

ENGINE INDICATING AND CREW ALERTING SYSTEM - PowerPoint Presentation

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Uploaded On 2023-10-30

ENGINE INDICATING AND CREW ALERTING SYSTEM - PPT Presentation

EICAS INTRODUCTION An engineindicating and crewalerting system EICAS is an integrated system used in modern aircraft to provide aircraft crew with aircraft engines and other systems instrumentation and crew annunciations ID: 1027210

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1. ENGINE INDICATING AND CREW ALERTING SYSTEM (EICAS)

2. INTRODUCTIONAn engine-indicating and crew-alerting system (EICAS) is an integrated system used in modern aircraft to provide aircraft crew with aircraft engines and other systems instrumentation and crew annunciations. EICAS typically includes instrumentation of various engine parameters, including for example revolutions per minute, temperature values, fuel flow and quantity, oil pressure etc.Typical other aircraft systems monitored by EICAS are for example hydraulic, pneumatic, electrical, deicing, environmental and control surface systems. EICAS has high connectivity & provides data acquisition and routing.

3. INTRODUCTIONEICAS is a key function of a glass cockpit system, which replaces all analog gauges with software-driven electronic displays. Most of the display area is used for navigation and orientation displays, but one display or a section of a display is set aside specifically for EICAS.The crew-alerting system (CAS) is used in place of the annunciator panel on older systems. Rather than signaling a system failure by turning on a light behind a translucent button, failures are shown as a list of messages in a small window near the other EICAS indications.

4. EICAS MODESEICAS categorizes displays and alerts according to function and usage into modes:Operational: Engine operating information and any alerts required to be actioned by the crew in flight. Only upper display presents information.Status: Provides details about the readiness of the aircraftMaintenance: Trouble-shooting and verification testing of the major sub-systems 

5. EICAS DISPLAY MESSAGESEICAS distinguishes 7 colors:White: all scales, normal operating range of pointers, digital readoutsRed: warning messages, maximum operating limit marks, digital readoutsGreen: thrust mode readout, selected EPR/N1(Engine Pressure Ratio/N1 compressor) speed marks or target cursorsBlue: testing of the system onlyYellow: caution and advisory messages, caution limit marks on scales, digital readoutsMagenta: during in-flight engine startingCyan: names of all parameters being measured and status marks

6. EICAS LEVELSLevel A warnings requiring immediate correction activityLevel B cautions requiring immediate crew awareness and possible activityLevel C advisories requiring crew awareness