DESCRIPTION
General 03−10−1
Central Display System 03−10−2
Crew Alerting Messages 03−10−3
Master Warning/Master Caution Lights 03−10−12
Aurals 03−10−13
Aural Warning Test 03−10−17
Aural Warning Panel 03−10−18
Inhibits 03−10−18
Central Aircraft Information and Maintenance System (CAIMS) 03−10−21
Flight Data Recorder 03−10−23
Stall Warning 03−10−23
Takeoff
Configuration Warnings 03−10−24
Landing Configuration Warning 03−10−25
EICAS Display 03−10−26
Systems Display (STAT Page) 03−10−27
Reversion Control Panel 03−10−28
PFD Reversion Control 03−10−29
PFD Reversion 03−10−30
EICAS Reversion Control 03−10−31
EICAS Reversion 03−10−32
SG Reversion Control 03−10−33
SG Reversion 03−10−34
EICAS Control Panel 03−10−37
Systems Reversion Control 03−10−38
Message Scrolling 03−10−40
Systems Synoptics 03−10−41
STAT Page 03−10−41
Bleed/AntiIce
Synoptic Page 03−10−42
Air Conditioning Synoptic Page 03−10−43
Hydraulic Synoptic Page 03−10−44
AC Electrical Synoptic Page 03−10−45
DC Electrical Synoptic Page 03−10−46
Fuel Synoptic Page 03−10−47
AURAL AND VISUAL WARNINGS
TABLE OF CONTENTS
CHAPTER 3
03−00−1
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
03−00−1
Page
TABLE OF CONTENTS
DESCRIPTION
Flight Controls Synoptic Page 03−10−48
Aural and Visual Warning EICAS Messages 03−10−49
EMS CIRCUIT PROTECTION
CB − Ind/Record System 03−20−1
CB − CAIMS System 03−20−2
AURAL AND VISUAL WARNINGS
TABLE OF CONTENTS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
03−00−2
Page
GENERAL
The aural and visual warning system provides indications to warn of potentially unsafe operating
conditions or airplane configurations, system malfunctions, and nonnormal
situations. Indications
can be generated by the following:
· Crew alerting subsystem
within the Engine Indication and Crew Alerting System (EICAS).
· Enhanced Ground Proximity Warning System (EGPWS).
· Weather Radar (WX) system.
· Traffic alert and Collision Avoidance System (TCAS).
· Altitude alert portion of the Air Data Computer (ADC).
· Stick shaker portion of the Stall Protection System (SPS).
EICAS provides crew with the necessary displays for airplane engine control and monitoring, control
surface monitoring and all major subsystem
synoptic displays. During normal operation, the engine
and control surface information is displayed on the EICAS display unit (DU3) and the system
synoptic information is displayed on the SYSTEMS display (DU4).
GF0310_001
DU 1 DU 2 DU 3 DU 4 DU 5 DU 6
PFD 1 MFD 1 EICAS SYSTEMS MFD 2 PFD 2
VS 2000
TOC
3
KSRP
180
220
210
200
170
160
150
0.88
0.856 M
190
KPHX
WX SAT
GSPD
−56
TAT
TAS
−40
234
345
LX
HDG
330
ETE 1+36
KLAX
TOC KPHX
KDVT KSRP
4000 4000
FL180
FMS1
DTK
360
20
20
10
10
20
20
10
10
33
30
W
24
21 15
12
E
6
3
0
1
2
1
2
3
VAPP VNAV
HDG AP1 ASEL 10400
29.92 IN
H23.4NM
SRP
BARO
9500
10500
10000
HDG
330
3
12.5NM
KDVT
LUF
KDVT
1300 5
1000
N
5
360
S
N
TERR
OFF
30
6
33
185
6
4
TOTALFUEL(LBS) 41550
1.54 1.54
73.3 73.3
789 789
14600 10000 14600
2350 ND
STAB
NU
NL RUDDER
LWD
NR
TRIMS
7.2
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
5750
115
81
93.4
5750
115
81
1.65 1.65
CRZ
EPR
SYNC
N1
ITT
OIL QTY (QTS)
ENG
APU
　
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