曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

 D.  Access to the E/E compartment is through the door behind the nose wheel or through the forward cargo compartment.
 TASK 24-41-04-004-001
 2.  External Power Contactor Removal (Fig. 401)________________________________
 A.  References
 (1)  
24-22-00/201, Manual Control

 (2)  
IPC 24-41-60 Fig. 1

 (3)  
IPC 24-41-60 Fig. 2

 (4)  
WDM 24-41-13, 24-41-23

 (5)  
SSM 24-41-01, 24-41-02

 B.  
Access

 (1)  
Location Zone 118 Electrical and Electronics Compartment, RH

 (2)  
Access Panel
 P714 Aux/Ext No. 1 Power Center
 P715 Aux/Ext No. 2 Power Center

 C.  
Procedure

 (1)  
Make sure all electrical power is off (Ref 24-22-00/201).

 S 014-004

 (2)  
Open the access door for the P714 panel (R12) or the P715 panel (R13).

 S 864-003
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-41-04
 ALL  ú ú 01 Page 401 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE B
SEE A EXTERNAL POWER CONTACTOR (TYPICAL)
SCREW  SCREW 
(4 PLACES)  (2 PLACES)  EXTERNAL 
EXTERNAL  POWER 
POWER  CONTACTOR 2 
CONTACTOR 1  (R13) 
SEE (R12) C  COVER  SEE  C 
SCREW 
(4 PLACES) 
NUT (6 PLACES) 
LOCKWASHER  P715 AUX/EXT 
P714 AUX/EXT  (6 PLACES)  NO. 2 POWER CENTER 
NO. 1 POWER CENTER  WASHER (6 PLACES)  B 
A 
ELECTRICAL 
CONNECTOR 
RECEPTACLE 

NOTE: TERMINAL LEADS NOT SHOWN FOR CLARITY. C
External Power Contactor InstallationFigure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-41-04
 ALL  ú ú 01 Page 402 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 034-005
 (3)  
Disconnect the electrical connector DR12 or DR13 from the contactor.

 S 034-028

 (4)  
Disconnect the electrical leads from the contactor:

 (a)  
Loosen the screws that attach the two terminal covers to the contactor.

 (b)  
Remove the terminal covers.

 (c)  
Remove the nuts and the washers that attach the six electrical leads to the terminal studs on the contactor.

 (d)  
Attach an identification tag to each electrical lead.

 (e)  
Remove the electrical leads from the terminal studs.

 S 024-029
 (5)  
Remove the external power contactor:

 (a)  
Remove the four screws that attach the contactor to the panel.

 (b)  
Remove the external power contactor from the panel.

 (c)  
Install the terminal washers, the terminal nuts, and the terminal cover.

 TASK 24-41-04-404-012
 3.  External Power Contactor Installation (Fig. 401)_____________________________________
 A. References
 (1)  
24-22-00/201, Manual Control

 (2)  
AMM 45-10-00/201, Central Maintenance Computer System

 (3)  
IPC 24-41-60 Fig. 1

 (4)  
IPC 24-41-60 Fig. 2

 (5)  
WDM 24-41-13, 24-41-23

 (6)  
SSM 24-41-01, 24-41-02

 B.
Access

 (1)  
Location Zone 118 Electrical and Electronics Compartment, RH

 (2)  
Access Panel
 P714 Aux/Ext No. 1 Power Center
 P715 Aux/Ext No. 2 Power Center

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-41-04
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) ELECTRICAL POWER 電源 2(96)