757 AMM 飞机维护手册 电源 ELECTRICAL POWER 2(60)

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BAT DISCH IND INHIBIT, C4286  1  * 
CIRCUIT BREAKER - MAIN/APU BATTERY TIE REMOTE  1  822, AFT EQUIP CTR RACK, E6  24-33-02
 CONTROL, M104916 
COMPUTER - (REF 31-41-00, FIG. 101) 
LEFT EICAS, M10181
 RIGHT EICAS, M10182
CONTACTOR - (REF 49-41-00, FIG. 101) 
APU CRANK, K117 

* SEE THE WDM EQUIPMENT LIST
Standby Power - Component Index
Figure 101 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH EXTENDED STANDBY POWER; ú 24-33-00
 ú ú 03 Page 102 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G38695
A

757
FAULT ISOLATION/MAINT MANUAL

STANDBY POWER
FIG. 
102 
COMPONENT  SHT  QTY  ACCESS/AREA  REFERENCE 
INVERTER - STATIC, M217  1  113AL, FWD EQUIP CTR 24-33-03 
LIGHT - APU BATTERY DISCHARE, YTGL3 2  1  FLT COMPT, P5, STANDBY POWER  * 
CONTROL PANEL, M10062 
2  FLT COMPT, P5, STANDBY POWER 
CONTROL PANEL, M10062 
2  FLT COMPT, P5, STANDBY POWER
 CONTROL PANEL, M10062 
PANEL - STANDBY POWER CONTROL, M10062 1  FLT COMPT, P5  24-33-04 
RELAYS - (REF 31-01-06, FIG. 101) 
AC STANDBY BUS OFF, K138
 AC STANDBY POWER, K105 24-33-01 
CTR BUS ISOL, K123
 DC STANDBY BUS OFF, K110 
EXT STBY PWR IND, K10416 
ISOL REQ, K122 
MAIN/APU BAT CHGR DET ENABLE, K10424
 MAIN BATTERY, K104 24-33-02 
MAIN BATTERY TRANSFER, K106  24-33-02 
STANDBY POWER, K109 24-33-01 
UNDER VOLTAGE SENSE, K113 
RELAY - (REF 31-01-86, FIG. 101)
APU BAT CHARGER DET, K10418 
APU START, K197 
BATTERY DISCHARGE INDICATION INHIBIT,
 K10422 
2  FLT COMPT, P5, STANDBY POWER
 CONTROL PANEL, M10062 
2  FLT COMPT, P5, STANDBY POWER
 CONTROL PANEL, M10062 

* SEE THE WDM EQUIPMENT LIST
Standby Power - Component Index
Figure 101 (Sheet 3)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH EXTENDED STANDBY POWER; ú 24-33-00
 ú ú 03 Page 103 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G38707
A

757
FAULT ISOLATION/MAINT MANUAL

STANDBY POWER
CONTROL PANEL, 
M10062  P11 PANEL 
SEE  A  BAT  STBY POWER 
P5 PANEL  AUTO 
ON  OFF  BAT 
w 
D I  a OFF  O 
S  F 
C  F 
aH  a 

STANDBY POWER CONTROL PANEL, M10062
P6 PANEL A
FLIGHT COMPARTMENT
ACCESS,
113AL
FORWARD EQUIPMENT
CENTER (LEFT SIDE)

SEE B
STATIC
INVERTER,
M217
MAIN BATTERY CHARGER (REF)
FWD
FORWARD EQUIPMENT CENTER (LEFT SIDE)
B
Standby Power - Component Location Figure 102 (Sheet 1)
G38582
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES WITH 30-MINUTE STANDBY POWER; ú 24-33-00
 ú ú 03 Page 104 ú May 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 FAULT ISOLATION/MAINT MANUAL
STANDBY POWER CONTROL PANEL, ACCESS, 113AL
M10062 P11 PANEL P5 PANEL
SEE A
P6 PANEL  BSEE CENTER (LEFT SIDE) FORWARD EQUIPMENT 
FLIGHT COMPARTMENT 
BAT DISCH OFF ON MAIN BAT APU BAT DISCHa a a  STBY POWER BATOFF AUTO  O F F a  (REF) BATTERY CHARGER MAIN  STATIC INVERTER, M217 
STANDBY POWER CONTROL PANEL, M10062 
A 

AFT CARGO
DOOR, 822

E6 RELAY 
APU BATTERY  PANEL 
CURRENT  (AFT OF  FWD 
MONITOR,  APU BATTERY) 
　
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