S 034-006
(5)
Disconnect the electrical connector from the ELCU.
S 024-007
(6)
Remove the bolts which hold the ELCU.
S 024-008
(7)
Remove the ELCU.
TASK 29-11-67-404-009
3. Install the Electrical Load Control Unit (ELCU) (Fig. 401)
_______________________________________________
A. References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
B. Access
(1)
Location Zones
119/120 Main Equipment Center
(2)
Access Panel
119BL Main Equipment Center
C. Procedure
S 424-010
(1)
Hold the ELCU in its position.
S 424-011
(2)
Install the bolts to hold the ELCU in its position.
(3)
Connect the electrical connector to the ELCU.
S 434-012
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-67
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
(4) S 434-013Connect the wires to the terminals on the ELCU. (a) Tighten to 120 - 125 inch-pound (13.0 - 14.1 newton-meters).
(5) S 414-014Close the power panel, P31 (P32), for the left (right) generator.
(6) S 864-015Supply electrical power (AMM 24-22-00/201).
(7) S 864-016Pressurize the applicable hydraulic system with the ACMP to do a check that the ELCU operates (AMM 29-11-00/201).
(8) S 864-017Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
(9) S 864-018Remove electrical power if it is not necessary (AMM 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-67
ALL ú ú 01 Page 404 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
GROUND SERVICING SYSTEM - DESCRIPTION AND OPERATION
___________________________________________________
1. General (Fig. 1)_______
A. The ground servicing system fills all hydraulic reservoirs from one location. The system components are in the aft left wing/body fairing. The system has a hand pump with suction line and a connection for pressure fill from a ground cart. There is also a remote quantity indicator, a fill selector valve, and a fill filter module.
2. Component Details (Fig. 1)_________________
A. Reservoir Manual Fill Pump
(1) The manual fill pump is a hand pump used to service the hydraulic reservoirs when pressure fill equipment is not available. The pump handle is stowed in brackets adjacent to the pump.
B. Suction Hose
(1) One end of the suction hose is connected to the manual fill pump. The other end is placed in a container of hydraulic fluid. When not in use, the free end of the hose is stowed in the pump handle.
C. Pressure Fill Connection
(1) The pressure fill connection is below the manual fill pump. This connection is used to pressure fill the reservoirs from a ground cart. A protective cap covers the connection when not in use.
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 液压 CHAPTER 29 - HYDRAULIC POWER 2(29)
