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Flight Crew Operating Manual
CSP A--013
MASTER
Engine Indication and Crew Alerting System --- General <MST>
Figure 02---20---1
Indicates Chapter in which information on item may be found.
Engine Indications
Fuel Flow
Engine Oil
N1 Vibration
Replaced by engine oil
pressure gauges during
engine start.
APU Gauges
Displayed only when
APU is running.
APU Inlet Door Status
MESSAGE AREA
FLIGHT NUMBER
Trim Indicators
Flight Compartment
Oxygen Pressure
Pressurization Data
Cabin Temperature
Brake Temperature
Landing Elevation
Pressurization Data
Gear Status
Flap Position
Fuel Quantity
MESSAGE AREA
Displayed only during
manual mode.
20
13
20
20
4
4
8
16
11
13
11
9
8
8
8
16
Status Page
Primary Page
Always displayed.
<0039>
<0006>
<0039>
<0039>
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND Vol. 1 02--20--4
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual MASTER
CSP A--013
EICAS Control Panel
Figure 02---20---2
EICAS Control Panel
Center Pedestal
Synoptic Pages
(ECS, HYD, ELEC, FUEL, F/CTL,
A/ICE, DOORS, MENU)
Used to display system synoptic pages.
A second push of the ELEC button will
replace the AC electrical synoptic page
with the DC electrical synoptic page.
STEP
Used to sequentially
UP and DN
Used to control operation
of the cursor on menu page.
The buttons slew the value
of selected items.
Indicates controls operable
during a panel failure.
Crew Alerting System (CAS)
Used when primary page is
displayed to remove caution
messages from view or display
additional caution messages if
more messages exist.
Status Page (STAT)
Used to display the
status page on ED2.
A second push will
remove status messages
from view or will display
additional status
messages if more
messages exist.
primary page on ED2.
Primary Page (PRI)
Used to displays the
step through the
pages on ED2.
Select (SEL)
Used to activate a
the menu page.
Cursor symbol, letter
or number will change
color to acknowledge
selection.
selected item on
Vol. 1 02--20--5
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual
CSP A--013
MASTER
EICAS Miscomparison Indication <MST>
Figure 02---20---3
CAS MISCOMP status (white)
Indicates that a miscomparison
of detected warning, caution or
aural alerts exists between
DCUs.
Status Page
<0039>
<0039>
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND Vol. 1 02--20--6
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual MASTER
CSP A--013
A. Display Reversion
If EICAS display 1 (ED1) fails, the primary page will be automatically displayed on ED2.
If ED2 fails, there is no automatic transfer to ED1. With either display failure, the
EICAS control panel is rendered inoperative. To regain control, the EICAS selector on
the SOURCE SELECTOR PANEL must be set to the operable display (ED1 or ED2) to
re-establish the EICAS control panel functions. The selector also makes available all
EICAS information on the selected display.
Display Reversion
Figure 02---20---4
Source Selector Panel
Center Pedestal
To ensure timely access to essential EICAS data, all EICAS pages can be made
available on either MFD by selecting the EICAS position on the respective Display
Reversionary Panel.
Display Selector
Figure 02---20---5
Pilot’s Display Reversionary Panel
Pilot’s Side Panel
Copilot’s Display Reversionary Panel
Copilot’s Side Panel
Vol. 1 02--20--7
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual
CSP A--013
MASTER
B. Aural Warning
Various tones call attention to warnings. There are ten types of aural alerts:
Sound Indication Chapter Reference
Warbler Stall Chapter 11, Flight Controls
Siren Windshear Chapter 18, Navigation
Whoop -- Whoop GPWS mode 1 or 2
(excessive descent rate or
excessive closure rate)
Chapter 18, Navigation
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