(c)  
Identify the wires on the RCCB for the installation.

 (d)  
Remove the RCCB with the remove - insert tool P/N 6500-001-0020.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EXTENDED STANDBY POWER ú

 24-33-02
 ú ú 02 Page 401 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 TASK 24-33-02-404-006
 3.  Install the Main-APU Battery Tie Remote Control Circuit Breaker_______________________________________________________________
 A. References
 (1)  AMM 24-22-00/201, Electrical Power - Control
 B. Access
 (1)  
Location Zones
 154 Aft Cargo Compartment (RIGHT)
 211/212 Flight Compartment

 (2)  
Access Panel
 822 Aft Cargo Compartment Door

 C. Install the RCCB
 S 864-007
 (1)  Do these steps to install the RCCB:
 (a)  
Put the RCCB in position in the aft equipment center rack, E6.

 (b)  
Install the screws that hold the RCCB.

 CAUTION:_______MAKE SURE YOU INSTALL THE WIRES CORRECTLY. DANGEROUS CIRCUIT MALFUNCTIONS CAN OCCUR IF YOU DO NOT INSTALL THE WIRES CORRECTLY.
 (c)  
Connect the wires to the RCCB with the remove - insert tool P/N 6500-001-0020.

 (d)  
Connect the battery connector to the APU battery.

 (e)  
Close the access cover on the forward side of the aft equipment center rack, E6.

 S 864-008
 (2)  Remove the DO-NOT-CLOSE tag and close this circuit breaker on the aft equipment center rack, E6:
 (a)  APU BAT CHGR
 S 864-009
 (3)  Remove the DO-NOT-CLOSE tag and close this circuit breaker on the main power distribution panel, P6:
 (a)  6L7, APU/MAIN BAT TIE
 S 864-010
 (4)  Remove the DO-NOT-CLOSE tag and close this circuit breaker on the overhead circuit breaker panel, P11:
 D. Do a Test of the RCCB Installation
 S 864-011
 (1)  Supply electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EXTENDED STANDBY POWER ú

 24-33-02
 ú ú 02 Page 402 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 864-012
 (2)  Make sure this circuit breaker on the main power distribution panel, P6, is closed:
 (a)  6D2, BAT XFR CONT
 S 864-013
 (3)  
Make sure these circuit breakers on the overhead circuit breaker panel, P11, are closed:

 S 714-014

 (4)  
Do a test of the RCCB, as follows:

 (a)  Do these steps at the standby power control panel on the pilots' overhead panel, P5: 1) Turn the STBY POWER switch to the BAT position. 2) Push the BAT switch to the ON position. 3) Make sure the APU BAT DISCH and MAIN BAT DISCH lights come
 on. 4) Push the BAT switch to the OFF position. 5) Turn the STBY POWER switch to the AUTO position. 6) Make sure the APU BAT DISCH and MAIN BAT DISCH lights go
 off.
 S 864-015
 (5)  Remove electrical power if it is not necessary (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EXTENDED STANDBY POWER ú

 24-33-02
 ú ú 02 Page 403 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 STATIC INVERTER - REMOVAL/INSTALLATION
______________________________________
 1.  General_______
 A.  The static inverter, M217 (referred to as the inverter) is on the left side of the forward equipment area.
 TASK 24-33-03-004-001
 2.  Remove the Static Inverter (Fig. 401)__________________________
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 電源 ELECTRICAL POWER 2(66)