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时间:2011-10-11 13:08来源:蓝天飞行翻译 作者:航空
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 S 014-003

 (2)  
Open the access door for the hydraulic service bay, 197KL, on the wing to body fairing (AMM 06-41-00/201).

 (3)
Move the handle for the fill selector valve to the OFF position.

 S 034-005

 (4)  
Disconnect the inlet and outlet hydraulic lines and install caps on the hydraulic lines.

 (5)  
Remove the two mount bolts.

 (6)  
Remove the filter module.


 S 864-004
 S 034-006
 S 024-007
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 29-18-04
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

LINES HYDRAULIC  ASEE BODY FAIRING AFT LEFT WING TO 
(2 LOCATIONS) MOUNT BOLT AND WASHER 
SELECTOR VALVE HANDLE FOR THE FILL 
FILTER FOR RESERVOIR FILL SEE B
FWD  OUTBD  BACKUP RINGS (2) BOWL O-RING OUTLET FILTER HEAD  ELEMENT O-RING BACKUP RING INLET 
A AFT LEFT WING TO BODY FAIRING  FILTER ELEMENT 
FILTER BOWL 
Filter Module for Reservoir Fill Figure 401  B 

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 29-18-04
 ALL  ú ú 01 Page 402 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 S 034-008
 (7) Remove the union from each filter module port.
 E. Remove the Filter Element (Fig. 401)
 S 014-009
 (1)  
Open the access door for the hydraulic service bay, 197KL, on the wing to body fairing (AMM 06-41-00/201).

 S 024-010

 (2)  
Remove the filter bowl from the filter head.

 S 024-011

 (3)  
Remove the filter element from the filter bowl.


 TASK 29-18-04-424-012
 3.  Install the Filter Module and the Filter Element________________________________________________
 A. General
 (1)  This task contains two procedures, one to install the filter module and one to install the filter element. Because this task contains two procedures, only the applicable group of steps must be done.
 To start one of these procedures, do the group of steps that is necessary to install the components. Then, do the "Put the Airplane Back to Its Usual Condition" group of steps.
 B. Consumable Materials
 (1)  D00054 Hydraulic System Lubricant - MCS 352
 C. References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 12-12-01/301, Hydraulic Systems

 (3)  
AMM 12-25-01/301, Exterior Cleaning


 D. Access
 (1)  Location Zones
 197 Wing to Body - Aft Lower Half (Left)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-18-04
 ALL  ú ú 01 Page 403 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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