(As installed)
Copyright . The Boeing Company. See title page for details.
August 1, 2003 6.20.21
Electrical -System Description
737 Operations Manual
Captain Instrument Panel
1
A/P A/T
P/RST P/RST TEST2
0 19
20700
21013 IN.HG. MB 992 3 6 5 4 ALT
BARO IASKNOTS 350380 43 B/CRS ILS OFF ILS
CHR
60 CTR
50 10 DME-1 DME-2 QTY TEST FUEL
TIME KGS ERR 7
40 20 ET/CHR 1 % 2
RESET HLD RUN 30 FS SS HLD RUN 1 FUEL FUEL
ERR 7 KGS ERR 7 KGS
% %
The standby power system utilizes the battery as a source of power to supply the following minimum essential instruments, communication, and navigation equipment:
CTR
- Left IRS
FUEL
- No. 1 RDMI
ERR
-
No. 1 VHF Navigation System (VOR, GS, and LOC) % KG.
-
No. 1 ADF Navigation System 1
FUEL FUEL
- No. 1 VHF Communications System
KG.
KG.
ERR ERR
- N1 & EGT Indication
% %
1
As installed
_______ AS SOON AS THE AIRPLANE LANDS, THE STANDBY POWER CAUTION: SWITCH SHOULD BE POSITIONED TO "BAT" TO ENERGIZE
THE ABOVE ELECTRONICS AND FOR VHF-1 COMMUNICATIONS.
NOTE: All of the Captain's instruments that are powered by standby power are integrally lighted on standby power.
Airplane Configuration - Inflight This illustration shows the Indicates Battery Switch - ON instruments which are useable Inoperative Standby Power Switch - AUTO with only the battery and Instruments standby busses powered.
(As installed)
Copyright . The Boeing Company. See title page for details.
6.20.22 August 1, 2003
Electrical -System Description
First Officer Instrument Panel
COCKPIT COMMUNICATION COCKPIT LIGHTS
Audio Selector Panels Standby Instrument Floodlight Flight Interphone White Dome Light Passenger Address System Magnetic Compass Light Service Interphone
Airplane Configuration - InFlight Standby Power Switch - AUTO Battery Switch - ON standby busses powered. with only the battery and instruments which are useable This illustration shows the Instruments Inoperative Indicates
(As installed)
Copyright . The Boeing Company. See title page for details.
August 1, 2003 6.20.23
Electrical -System Description
737 Operations Manual
Captain Instrument Panel
EADI
M
MACH 60 77 400 350 8 100 31 700 9 8 2 10
VMO 120 IN OP 7 3MB IN.HG ALT
KNOTS 140 160 250 300 285 10 6 5 4 99213 2
200 180
PULL TO SET
CHR 40 50 DAY MO/YR60 ET/CHR 20 10 GMT DATE DME-1 DME-2 EHSI SPEED 0 1000 FPM 1 1 2 2 4 4 6 .5 .5 VERTICAL 0700 BARO ALT 9 6 5 4 3 2 0 1 350380 43 IASKNOTS 992 MB IN.HG. 1013 2 TEST QTY % FUEL KG. ERR CTR
RUN HLD 30 FUEL FUEL
RESET KG. KG.
ERR ERR
% %
The standby power system utilizes the battery as a source of power to supply the following minimum essential instruments, communication, and navigation equipment:
-
Left IRS
-
No. 1 RDDMI (IRS Switch - Both ON L)
-
Standby Horizon Indicator
-
No. 1 VHF Navigation System (VOR, GS, and LOC)
-
No. 1 ADF Navigation System
-No. 1 VHF Communications System
-
No. 1 Air Data Computer
-
N1, N2, EGT and Fuel Flow
CAUTION: AS SOON AS THE AIRPLANE LANDS, THE STANDBY POWER SWITCH SHOULD BE POSITIONED TO "BAT" TO ENERGIZE THE ABOVE ELECTRONICS AND FOR VHF-1 COMMUNICATIONS.
NOTE: All of the Captain's instruments including the engine and fuel quantity indicators, that are powered by standby power are also integrally lighted by standby power.
Airplane Configuration - Inflight This illustration shows the Indicates Battery Switch - ON instruments which are useable Inoperative Standby Power Switch - AUTO with only the battery and Instruments standby busses powered.
(As installed)
Copyright . The Boeing Company. See title page for details.
6.20.24 August 1, 2003
Electrical -System Description 737 Operations Manual
First Officer Instrument Panel
COCKPIT COMMUNICATION COCKPIT LIGHTS
Audio Selector Panels Standby Instrument Floodlight Flight Interphone White Dome Light Passenger Address System Magnetic Compass Light
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本文鏈接地址：737-300機組操作手冊Flight Crew Operations Manual FCOM 2(53)
