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Figure 02 ---20 ---2
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CAS MISCOMP status (white)
Indicates that amiscomparison of detected warning, caution or auralalerts exists between DCUs.
Status Page
EICAS Miscomparison Indication <MST>
Figure 02---20---3
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A. Display Reversion
IfEICASdisplay1(ED1)fails, theprimarypagewillbe automaticallydisplayed on ED2. IfED2fails, there is no automatic transferto ED1. With eitherdisplayfailure, the EICAS controlpanelis renderedinoperative. To regain control, theEICAS selector on the SOURCESELECTORPANEL mustbe setto the operable display (ED1 orED2)to re-establishtheEICAS controlpanelfunctions. The selectoralso makes available all EICASinformation onthe selected display.
Display Reversion
Figure 02 ---20 ---4
To ensure timely access toessentialEICASdata,allEICASpages can be made available on eitherMFDby selectingthe EICASposition on the respective Display ReversionaryPanel.
Pilot’s Display Reversionary Panel Copilot’s Display Reversionary Panel
Pilot’s Side Panel Copilot’s Side Panel
Display Selector
Figure 02 ---20 ---5
Flight Crew Operating Manual MASTER
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AURAL/VISUAL INDICATING AND RECORDING Vol. 1 02-
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Engine Indication and Crew Alerting System REV 56, Jan 31/03
B. Aural Warning
Various tonescallattention to warnings. There are tentypesof auralalerts:
Sound Indication Chapter Reference
Warbler Stall Chapter 11, Flight Controls
Siren Windshear Chapter 18, Navigation
Whoop -
Whoop GPWS mode1or 2 (excessive descent rate or excessive closure rate) Chapter 18, Navigation
Fire Bell Fire warnings Chapter 10, Fire Protection
Clacker 1. Excessive stabilizer trim tm
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t 2. VMO/MMO exceedance 3 Ai d t hi h f3. Airspeed too high for current flap setting Chapter 11, Flight Controls Ch p 12 Fligh ICha
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Cavalry Charge Autopilot disconnect Chapter 3, Automatic Flight Control System
Horn Gearnot down Chapter16, Landing Gear
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