S 794-032

 (2)  
Make sure there are no air leaks at the air line connections on the module.

 S 864-033

 (3)  
Remove pneumatic power if it is not necessary (AMM 36-00-00/201).

 S 414-034

 (4)  
Close the access doors, 193HL and 194ER, for the environmental control system (AMM 06-41-00/201).

 TASK 29-11-16-404-035
 5. Install the Filter Element in the Reservoir Pressurization Module
_________________________________________________________________
 A. Consumable Materials
 (1)  
D00054 Hydraulic System Lubricant - MCS 352

 (2)  
D00090 Trichlorethane 1, 1, 1

 (3)  
A00363 Sealant - RTV 162

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 29-11-16
 ALL  ú ú 01 Page 404 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 (4)  A00247 Sealant - Chromate Type, BMS 5-95
 B. References
 (1)  
AMM 06-41-00/201, Fuselage Access Doors and Panels

 (2)  
AMM 36-00-00/201, Pneumatic - General

 C. Access
 (1)  
Location Zone
 135/136 Wing Center Section
 139 Forward Section of Keel Beam
 193/194 Wing to Body Fairings

 (2)  
Access Panels
 193HL ECS Components (Left)
 194ER ECS Components (Right)

 D. Install the Filter Element (Fig. 401)
 S 144-037
 (1)  
Remove the sealant remaining on the filter cap and the adjacent surface of the reservoir pressurization module.

 S 114-038

 (2)  
Clean the hole in the reservoir pressurization module for the filter element.

 S 114-039

 (3)  
Clean the filter element with solvent and fully dry the filter element.

 S 644-040

 (4)  
Apply the hydraulic lubricant or the hydraulic fluid to the new O-rings and the threads of the filter cap.

 S 434-041

 (5)
Assemble the filter element, the O-rings and the filter sleeve.

 S 424-043

 (6)  
Install the filter element assembly in the reservoir pressurization module.

 (7)
Install the filter cap on the reservoir pressurization module.

 (8)  
Safety the filter cap with a lockwire.

 S 394-047

 (9)  
Apply a bead of sealant to the joint between the filter cap and the reservoir pressurization module.
　
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