• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-20 08:05来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (2)  
AMM 27-61-00/201, Spoiler/Speedbrake Control System


 B.  Access
 (1)  Location Zone
 211/212 Flight compartment

 C.  Prepare for Removal
 S 864-001
 WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN
_______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
 (1)  
Do the deactivation procedure for the spoilers (AMM 27-61-00/201) or move all persons and equipment away from the spoilers.

 S 864-002

 (2)  
Remove electrical power (AMM 24-22-00/201).

 S 864-003

 (3)  
Open this circuit breaker on the main power distribution panel (referred to as the P6 panel) and attach a DO-NOT-CLOSE tag:


 (a)  6A6, DC BUS TIE CONT
 S 014-004
 WARNING: REMOVE ALL ELECTRICAL POWER FROM THE AIRPLANE BEFORE YOU OPEN THE
_______ P6 PANEL. VOLTAGES IN THE P6 PANEL CAN CAUSE SERIOUS INJURY TO PERSONS
 (4)  Open the P6 panel.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-03
 ALL  ú ú 01 Page 401 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL


MAIN P0WER DISTRIBUTION PANEL P6
A DC Tie Control Unit Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-03
 ALL  ú ú 01 Page 402 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 D. Remove the DC Tie Control Unit
 S 024-006
 (1)  Do these steps to remove the DC tie control unit:
 (a)  
Remove the electrical connector from the DC tie control unit.

 (b)  
Remove the four screws that hold the DC tie control unit.

 (c)  
Remove the DC tie control unit.


 TASK 24-32-03-404-007
 3.  Install the DC Tie Control Unit (Fig. 401)_______________________________
 A. References
 (1)  
AMM 24-22-00/201, Electrical Power - Control

 (2)  
AMM 27-61-00/201, Spoiler Speedbrake Control System


 B. Access
 (1)  Location Zone
 211/212 Flight compartment

 C. Install the DC Tie Control Unit
 S 424-008
 (1)  Do these steps to install the DC tie control unit:
 (a)  
Put the DC tie control unit in position in the P6 panel.

 (b)  
Install the four screws that hold the DC tie control unit.

 (c)  
Connect the electrical connector to the DC tie control unit.


 S 434-009
 (2)  
Close the P6 panel.

 S 864-010

 (3)  
Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P6 panel:


 (a)  6A6, DC BUS TIE CONT
 D. Do a Test of the DC Tie Control Unit Installation.
 S 864-011
 (1)  Supply electrical power (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 24-32-03
 ALL  ú ú 01 Page 403 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 (2)  S 864-012Make sure these circuit breakers on the P6 panel are closed: (a) 6C11, L DC VOLT SENSE (b) 6D9, TIE L (c) 6H9, TIE R (d) 6H10, R DC VOLT SENSE
 (3)  S 864-034Make sure the L TRU circuit breaker on the P6 or P31 panel is closed: (a) 6C17 or 31EE2, L TRU
 (4)  S 864-045Make sure the R TRU circuit breaker on the P6 or P32 panel is closed: (a) 6C23 or 32EE2, R TRU
 (5)  S 864-013Make sure the six EICAS circuit breakers on the overhead circuit breaker panel (referred to as the P11 panel) are closed:
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 电源 ELECTRICAL POWER 2(51)