MB 5 IN HG
120
V
MO
ALT
O
LOW 129923 013
7
U
MB IN.HG
300
OUTER T
10 3
12992 250 KNOTS
E
A/S
R
140
4
6 160
250 300
5
IAS KNOTS
200180
10 PULL TO SET
12 2
.
VERTICAL 4CHR DATE SPEED
120
51558
60 0
OFF
6
DME-1 DME-2
4
V V
10
1000 FPM
OO
50
.5 4
RR TIME
1 2
ET/CHR ADF ADF
2040
EHSI
RUN 30 RUN
HLD HLD
SS
FS

RESET
5
90 1
10
7 750
8 2
7 METER 3
10 6
ADF INOP
mb
6 1013 4
1
NOSE WHEEL STEERING
6
N
REGISTRATION
A
O
T

L
TERR WXR M R
SELCAL
ON ON
1510 +
PANEL BACKGROUND
AFDS FLOOD
14
WIND-SHIELD
AIR

OFF OFF
OFF
FOOT AIR
1
1 3
CHR DATE
60 CHR
50

2
6010 4
DME-1 DME-2
TIME 50
10
TIME ET/CHR
40 20
ET/CHR
RUN
40 20
RUNHLD 30 HLD
SS
FS

30
RUNRUN
RESET HLD HLD
SS
FSRESET
# As installed
Circled numbers refer to chapters where information on the item may be found.
The controls, panels, and indicators shown in this chapter are representative of installed units and may not exactly reflect the details of the latest configuration. Refer to the corresponding chapter under system descriptions for current information.
Copyright . The Boeing Company. See title page for details.
June 4, 2004  1.20.5
Airplane General, Emergency Equipment, Doors, Windows -Instrument Panels
737 Operations Manual
First Officer’s Instrument Panel
4 11 10
15

1
A/P A/T FMC
P/RST P/RST P/RST
TEST2
PULL UP
4
INST
SWITCH
BELOW G/S
P-INHIBIT
ALTITUDE ALERT
10
A I
EADI
0
R
AIRWAYS W
A
60 Y
31
S
19
2
80
400 MACH
700
7
M I
8
8
MIDDLE D
100
D
10
TAT
7
32 10
L
ALT350
7
E
MB IN.HG
C
KT
380 120 1013 292
9
O
6
4
U
SAT TAS OUTER T
300
E
5
R
270
140
250 KNOTS
160

5
200180
CHR DATE
1 PULL TO SET
602
3
1
HYD BRAKE
PRESS .5 VERTICAL 4
14
4
50 10
SPEED 2 TIME
0 6
PSI X 1000
1250 1558
ET/CHR 1
1000 FPM
0 10
DME-1
40
20
DME-2 .5 4
1 RUN
RUN
2 30
HLD HLD
SS
FSRESET
3
HYD SYS
PRESS

4
EHSI
6
13
0 +
PSI X 1000
TERR WXR
1
ON ON

10
ADF INOP
1
3

1
232
1 HYD QTY RFL 4 1 HYD QTY 4RFL
10 15
44
6
10
REGISTRATION
SYS A F SYS B F
EE
SELCAL
PANELGROUND PROXIMITY
3
FLAP/GEAR
INHIBIT

INOP
WIND-SHIELD
AIR

OFF
SYS TEST
NORMAL
FOOT AIR
1
15 3
GROUND PROXIMITY GROUND PROXIMITY
3
CHR
5
3
2
FLAP
FLAP GEAR INHIBIT
60
3 INOP
INOP
INHIBIT INHIBIT HYD BRAKE
PRESS
14
4
2

50 10
TIME
0
PSI X 1000
ET/CHR 1 SYS TEST
SYS TEST
40 20
NORMAL NORMAL NORMAL
RUN RUN
30
HLD HLD
3
SS FSRESET
GROUND PROXIMITY
FLAP GEAR TERR INOP
INHIBIT INHIBIT INHIBIT
# SYS TESTAs installed
NORM NORM NORM
Circled numbers refer to chapters where information on the item may be found.
Copyright . The Boeing Company. See title page for details.
1.20.6  June 4, 2004
Airplane General, Emergency
 
Equipment, Doors, Windows -Instrument Panels
737 Operations Manual
Center Instrument Panel and Lightshield (Non–EIS Airplanes)
FLT CONT ELEC ANTI-ICE ENG
　
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本文鏈接地址：737-300機組操作手冊Flight Crew Operations Manual FCOM 1(81)