(a)
Filter module for the pressure and the case drain of the alternating current motor pump (ACMP), referred to in this procedure as the filter module
(b)
Filter elements
(c)
Differential pressure indicators
(d)
Pressure switches
(e)
Check valves.
(2)
To start one of these procedures, do the "Prepare for Removal" group of steps. Then, do the applicable group of steps that is necessary to remove the component.
B. References
(1)
AMM 06-41-00/201, Fuselage Access Doors and Panels
(2)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
C. Access
(1)
Location Zone
197 Wing to Body - Lower Half (Left)
(2)
Access Panels
197KL Central Hydraulic Service Center
D. Prepare for the Removal
S 864-002
(1)
Open the access door, 197KL, for the central hydraulic service center (AMM 06-41-00/201).
S 864-003
(2)
Remove the pressure from the center hydraulic system and the reservoir (AMM 29-11-00/201).
S 864-004
(3)
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:
(a)
11K15, HYDRAULICS ELEC PUMP C1
(b)
11K24, HYDRAULICS ELEC PUMP C2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-19
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
E. Remove the Filter Module (Fig. 401)
S 034-005
(1) Disconnect the electrical connectors from the pressure switches on the filter module.
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 1(224)