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Standby Power Switch   - AUTO Battery Switch   - ON Airplane Configuration - In Flight  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  6.20.25
Electrical -System Description

Electrical System Power Distribution No. 1 Generator Inoperative
Failure In Flight, Transfer Busses Normal
Inoperative Components  Indication 
No.1 tank forward fuel pump Center tank right fuel pump  LOW PRESSURE light LOW PRESSURE light 
Galley(s)  Inoperative 
No.1 Generator Generator bus No. 1  GEN OFF BUS light BUS OFF light 
Left forward window heat Right side window heat Left No., 4 & 5 window heat  ON light – extinguished ON light – extinguished Inoperative 
Left elevator pitot heat  L ELEV PITOT light 
System B electric pump  LOW PRESSURE light 
Left outboard landing light Right inboard landing light Left runway turnoff light Nose gear taxi light  Inoperative Inoperative Inoperative Inoperative 
Equipment cooling normal  OFF light 

Copyright . The Boeing Company. See title page for details.
6.20.26  August 1, 2003

Electrical -System Description
No. 2 Generator Inoperative
Failure In Flight, Transfer Busses Normal
Inoperative Components  Indication 
No.2 tank forward fuel pump Center tank left fuel pump Fuel temperature indicator  LOW PRESSURE light LOW PRESSURElight Inoperative 
Galley(s)  Inoperative 
No.2 Generator Generator bus No. 2 TR unit No. 3  GEN OFF BUS light BUS OFF light TR No. 3 voltage – Zero 
Left side window heat Right forward window heat Right No., 4 & 5 window heat  ON light – extinguished ON light – extinguished Inoperative 
Right elevator pitot heat TEMP PROBE Heat  R ELEV PITOT light TEMP PROBE light 
System A electric pump  LOW PRESSURE light 
Right outboard landing light Left inboard landing light Runway turnoff light  Inoperative Inoperative Inoperative 
Equipment cooling – Alternate  If switch is to alternate, OFF light 
Recirculation Fan  Inoperative 
Engine vibration amplifier (non-EIS)  Inoperative 

Copyright . The Boeing Company. See title page for details.
August 1, 2003  6.20.27
Electrical -System Description 737 Operations Manual

Intentionally
Blank

Copyright . The Boeing Company. See title page for details.
6.20.28  August 1, 2003

737 Operations Manual

Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.1
Engine Instrument System (EIS) Primary Panel  . . . . . . . . . . . . .  7.10.1 Reverser Unlocked, Autothrottle Limit, and Thrust Mode Display  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.2 N1 Indications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.3 N1 Manual Set Knob  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.4 EGT Indications  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.4 N2 Indications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.5 Fuel Flow/Fuel Used Indications  . . . . . . . . . . . . . . . . . . . . . .  7.10.6 Engine Instrument System (EIS) Secondary Panel . . . . . . . . . . .  7.10.8 Caution Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .  7.10.9 Total Air Temperature Indication  . . . . . . . . . . . . . . . . . . . . . .  7.10.9 Engine Oil Indications  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.10 Engine Vibration Indications  . . . . . . . . . . . . . . . . . . . . . . . .  7.10.11 Hydraulic System Pressure and Quantity Indications . . . . . .  7.10.11
Conventional Engine Instruments Primary Panel  . . . . . . . . . . . 7.10.12 Reverser Unlocked Light  . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.13 N1 Indications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.13 EGT Indications  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.14 N2 Indications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.15 Fuel Flow/Fuel Used Indications  . . . . . . . . . . . . . . . . . . . . . 7.10.15
Conventional Engine Instruments Secondary Panel  . . . . . . . . . 7.10.17 Engine Oil Quantity Test Switch  . . . . . . . . . . . . . . . . . . . . . 7.10.18 Caution Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.18 Engine Oil Indications  . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.10.19 Engine Vibration Indications  . . . . . . . . . . . . . . . . . . . . . . . . 7.10.20
　
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本文鏈接地址：737-300機組操作手冊Flight Crew Operations Manual FCOM 2(54)