EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-01
 ALL  ú ú 03 Page 401 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE A
TRU 4 (T1497) 
TRU 1 (T1494)  TRU 2 (T1495) BSEE  TRU 3 (T1496) BSEE  SEE  B 
SEE  B 

E-30 EQUIPMENT RACK
A

MAIN TRU (TYPICAL)
B
Main Transformer Rectifier Unit (TRU) Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-01
 ALL  ú ú 01 Page 402 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  P180 DC Power Distibution Panel
 1) 180A11 DC 1 TRU 1 BUS TIE
 2) 180A14 DC 2 TRU 2 BUS TIE
 3) 180A26 DC 3 TRU 3 BUS TIE
 4) 180A28 DC 4 TRU 4 BUS TIE

 S 024-003
 (2)  Remove the applicable TRU from the E-30 equipment rack (Ref 20-11-22/401).
 TASK 24-32-01-404-004
 3.  Main Transformer Rectifier Unit Installation (Fig. 401)____________________________________________
 A. References
 (1)  
20-11-22/401 Rack-Mounted Electrical/Electronic Module

 (2)  
24-22-00/201, Manual Control

 (3)  
45-10-00/201, Central Maintenance Computer System

 (4)  
AMM 45-10-00/201, Central Maintenance Computer System

 (5)  
IPC 24-32-01 Fig. 1

 (6)  
WDM 24-32-11, 24-32-12

 (7)  
SSM 24-32-01

 B.
Access

 (1)  
Location Zone 116 Area Between Nose Gear Well and Fuselage, RH

 C.
Install the Main TRU

 S 424-005
 (1)  
Install the applicable TRU in the E-30 equipment rack (Ref 20-11-22/401).

 (a)  
Tighten the terminal nuts to 90 to 110 pound-inch.

 S 864-006
 (2)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers for the applicable TRU:

 (a)  
P6 Power Distribution Panel
 1) 6A5 TRU 1

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-01
 ALL  ú ú 04 Page 403 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 2) 6A14 TRU 2
 3) 6A23 TRU 3
 4) 6A32 TRU 4

 (b)  P180 DC Power Distibution Panel
 1) 180A11 DC 1 TRU 1 BUS TIE
 2) 180A14 DC 2 TRU 2 BUS TIE
 3) 180A26 DC 3 TRU 3 BUS TIE
 4) 180A28 DC 4 TRU 4 BUS TIE

 D. Do a Test of the Main TRU
 S 864-010
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 714-009

 (2)  
Do a test of the main TRU.

 (a)  
Get access to the EXISTING FAULTS page for Chapter 24 (if any) on the CMCS.

 (b)  
Make sure the CMCS messages for the applicable main TRU do not show (AMM 45-10-00/201).

 (c)  
Get access to the maintenance page for the electrical system (AMM 45-10-00/201).

 (d)  
Make sure the DC Volts and DC Amps values are in the correct range.

 (3)  
Remove electrical power, if it is not necessary (Ref 24-22-00/201).

 S 864-011
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-01
 ALL  ú ú 03 Page 404 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 ELECTRICAL POWER 電源 2(74)