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AC BUS 2
V
KVA
GEN
2
GEN
1
AC ESS BUS
AC BUS 4
AC BUS 3
V
KVA
V
KVA
GEN
3
GEN
4
0 0 0
0 0 0
115
400
V
HZ
RAT GEN
DC ELECTRICAL
AC BUS 2
FEEDER
DC BUS 1
-10°C
AC BUS 1
FEEDER
DC ESS BUS
ESS
TRU 1
AC ESS
BUS
BATT BUS
DC EMER
BUS
AV BATT
DIR BUS
AV
BATT
20°C
APU
BATT
APU BATT
DIR BUS
ESS
TRU 2
AC BUS 3
FEEDER
DC BUS 2
TRU 1 TRU 2
0
0
V
A
26
0
24
0
V
A
V
A
0
0
V
A
28
75
V
A
0
0
V
A
RAT GEN
GX_06_034
CHARGER CHARGER
For Training Purposes Only
Sept 04
6-35
P I LOT T R A I N I N G GU I D E
ELECTRICAL
EMERGENCY DC POWER
In the event of loss of all AC power, or the airplane speed is 147 knots or less with the
RAT deployed, a BATTERY EMER PWR ON EICAS message will be displayed. If
the RAT is deployed and speed is less than 147 knots, the RAT GCU will
automatically shed RAT electrical output, giving priority to hydraulics.
DC ELECTRICAL
AC BUS 2
FEEDER
DC BUS 1
-10°C
AC BUS 1
FEEDER
DC ESS BUS
ESS
TRU 1
AC ESS
BUS
BATT BUS
DC EMER
BUS
AV BATT
DIR BUS
AV
BATT CHARGER CHARGER
20°C
APU
BATT
APU BATT
DIR BUS
ESS
TRU 2
AC BUS 3
FEEDER
DC BUS 2
TRU 1 TRU 2
0
0
V
A
26
24
24
24
V
A
V
A
0
0
V
A
0
0
V
A
0
0
V
A
AC ELECTRICAL
00
0
V
KVA
HZ
GEN
APU
AC BUS 1
00
V
KVA
AC BUS 2
V
KVA
GEN
2
GEN
1
AC ESS BUS
AC BUS 4
AC BUS 3
V
KVA
V
KVA
GEN
3
GEN
4
0 0 0
0 0 0
0
400
V
HZ
RAT GEN
GX_06_035
147
180
170
160
150
140
130
120
147
8
6
NOTE:
Battery emergency power is available for a minimum of 15 minutes.
BATTERY EMER PWR ON
6-36 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRICAL
DC POWER EMERGENCY OVERRIDE
In the event of loss of all DC power, selecting the DC POWER EMERGENCY
OVERRIDE switch (located on the pedestal) to OVERRIDE, will allow ESS TRU 1
and 2 to bypass the DCPC and power the SPDAs directly. All components normally
powered by the DC ESS BUS and the BATT BUS will be powered directly from the
ESS TRUs.
ELECT DC PWR
EMER OVRD
OVRD
NORM
20
10
30
20
10
30
0
9
8
7
6
5
4
3
2
1
100FEET
ALT
1 000 32
4
10 13
mb/hPa
29 9 2
IN HG
IAS KNOTS
180 200 220 250
BARO
Honeywell Honeywell Honeywell Honeywell
WX
ET
NO BEARING
RA 9 . 8NM +13
TA4 . 5NM -04
SAT
GSPD
TERR
-56
TAT
TAS
-40
234
345
INHIB
LX
00 : 10 0 . 05L
HDG MAG2
315
ETE 1+36
12 . 5
KDVT
NM
FL
BELOW
TCAS TEST
360 FMS1
N
5 5
3
6
33
30
- 02
- 02
+ 12
- 04
KABC
KKLM
KKLM
TOC
TOC
KGHJ
KGHJ
LUF
KDEF
KDEF
4000 4000
FL180
+ 09
TOTAL FUEL (LBS) 25750
1.02 1.02
25.4 25.4
443 443
12950 0 12800
0
ND
STAB
NU
NL RUDDER
LWD RWD
NR
AIL
– TRIMS –
6.0
N2
FF (PPH)
OIL TEMP
OIL PRESS
61.4
690
75
51
61.4
690
80
49
1 . 64 1 . 64
98.5 98.5
T/O
EPR
N1
ITT
GEAR
PARK/EMER BRAKE ON
NO TAKEOFF
IGN
START START
IGN
IN
0
DN DN DN
END
Honeywell
1300
0.00
0
0
90
13 13
20
19 20
22 22
20
OXYGEN
AFT
CABIN (°C)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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