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V
A
0
0
ESS
TRU 1
SHED
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
RES
RPM EGT
10.4
22
1300
85 %
0.00
20
100 400
4.5
5.0
10.4
CKPT (5C)
OXYGEN
CAB ALT
CAB RATE
P
FWD
APU
RWD
CABIN (5C)
AFT
CABIN (5C)
21
29
23
20
"1300
LDG ELEV 1000
NOTE
ELECTRICAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−10−44
EICAS PHILOSOPHY
The following represents the EICAS symbols and logic for the AC and DC synoptic pages. The
symbols are shown in serviceable and failure conditions.
EXT
AC
V
KVA
HZ
115
400
28
ON
EXT
DC VA
28
12
ELECTRICAL SYSTEM LOGIC
BUS
POWERED
GEN
ENGINE
FAILED
NOT
POWERED
TRU "s
INVALID
APU
OPERATING
NOT
OPERATING
BATTERIES
FAILED INVALID
RAT RAT GEN RAT GEN RAT GEN RAT GEN
AVAILABLE FAILED INVALID
V
KVA
HZ
115
400
0
V
KVA
HZ
0
0
0
V
KVA
HZ
0
0
0
EXT AC
EXT DC
28VA
12
EXT
DC VA
24
12
EXT
DC VA
24
12
GF0710_056
EXT
AC
EXT
AC
EXT
DC
AC
EXT
ELECTRICAL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
07−10−45
ELECTRICAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−10−46
THIS PAGE INTENTIONALLY LEFT BLANK
COCKPIT CIRCUIT BREAKER PANEL (CCBP)
E
1 2 3 4 6 7 8 9 10 11 12 13 14
TRIM
STAB
TRU 2
ESS
F
1 2 4 5 6 7 8 9 10 11 12 13 14
G
1 2 3 4 5 6 7 8 9 10 11 12 13
H
1 2 3 4 5 6 7 8 9 10 11 12 13
SLAT/
PWR 2
FLAP TRU 1
ESS
RAT
MONITOR
V/F
AC BUS 4
MONITOR
20
5
15 15 15
HT 1
TAT
HEAT
L AOA
3
HT B
PITOT 1
HT
PITOT 3
DETECTOR
L ICE
HEAT
R AOA
HT 2
TAT STBY
HT
PITOT
15
WINDOW
L
TRU 1
ESS
L
HEAT 1
WSHLD
FLAP/
PWR 1
SLAT BAY
TRU
A/T
HT A
PITOT 1
DETECTOR
R ICE
HEAT A
R AOA
20
L
HEAT 2
WSHLD
20
FREQ
SATCOM
CH 2
CTLR
HEAT 2
B
1 2 3 4 5 6 7 8
7.5
HT WINDOW
1 2 3 4 5 6
TRU 2
7 8
1 2 3 4 5 6 7 8
RCCB
9 10
PITOT 2 R
C
D 0.5
CHGR
AV BATT
BATT
AV
RCCB
BATT
APU
HEAT
AV BATT
HT 3
TAT
HEAT 1
WSHLD
R
HEAT 2
WSHLD
R
0.5 5 5 20 20
15
HEAT
1 2 3 4 5 6
TRU 1
A
AC BUS 2
AC BUS 3
DC
AC ESS BUS
AC BUS 1
FAN
B HEAT
ALT
[1]
STBY
ADI
[1] On airplane 9105 and subsequent and airplane incorporating Service Bulletin SB 700−34−022.
　
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