S 024-007
(3)
Remove the bolts and washers and remove the return filter module.
F.
Remove the Filter Element (Fig. 401)
S 034-008
(1)
Remove the filter case from the return filter module.
S 024-009
(2)
Remove the filter element from the return filter module.
G.
Remove the Return Filter Module Components (Fig. 401)
NOTE: The steps which follow are applicable to the check valves, the
____ relief valve, the differential pressure indicator, and the ground service connector.
S 024-010
(1)
Loosen and remove the component from the return filter module.
S 034-011
(2)
Install a plug in the opening in the return filter module.
TASK 29-11-13-404-012
3. Install the Center System Return Filter Module and Components
_____________________________________________________________
A. General
(1)
This task contains three procedures which install the components which follow:
(a)
Return filter module for the center system
(b)
Filter element
(c)
Filter module components which are the check valves, the relief valve, the indicator for differential pressure, and the ground service connector.
(2)
To start one of these procedures, do the applicable group of steps that is necessary to install the component. 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
(4)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
D.
Access
(1)
Location Zones
197 Wing to Body - Aft Lower Half (Left)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
29-11-13
ALL ú ú 01 Page 404 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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