(2)
AMM 12-12-01/301, Hydraulic Systems
(3)
AMM 12-25-01/301, Exterior Cleaning
C. Access
(1)
Location Zones 197 Wing to Body - Aft Lower Half (Left) 211/212 Control Cabin
(2)
Access Panel
197KL Central Hydraulic Service Center
D. Install the Selector Valve (Fig. 401)
S 644-011
(1)
Apply hydraulic lubricant or hydraulic fluid to the O-rings and the threads on the unions and the check valve.
S 434-012
(2)
Install new O-rings on the unions and the check valve.
S 434-013
(3)
Install the check valve in the selector valve port at the center system connection point.
S 434-014
(4)
Install the unions in the valve ports for the left and right system connection points.
S 424-015
(5)
Put the selector valve in its position and install the mount bolts and washers.
(6)
Tighten the mount bolts to 72-88 pound-inches.
S 434-016
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(7) S 434-017Remove the caps from the hydraulic lines and connect them to the selector valve.
(8) S 434-018Connect the electrical connector to the selector valve.
(9) S 864-019Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11: (a) 11K19, HYDRAULICS QTY CTR (b) 11K20, HYDRAULICS QTY LEFT (c) 11K21, HYDRAULICS QTY RIGHT
S 864-020
(10)
Pressurize the reservoir fill system (AMM 12-12-01/301). S 214-021
(11)
Make sure there are no leaks at the connection points to the selector valve.
S 104-022 CAUTION: QUICKLY CLEAN THE INSTALLATION AREA OF ALL HYDRAULIC FLUID.
_______ HYDRAULIC FLUID CAN CAUSE DAMAGE TO THE AIRPLANE EQUIPMENT.
(12)
Clean all hydraulic fluid from the installation area (AMM 12-25-01/301).
S 414-023
(13)
Close the access door for the hydraulic service bay, 197KL (AMM 06-41-00/201).
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RESERVOIR FILL INDICATOR - REMOVAL/INSTALLATION
_______________________________________________
1. General
_______
A. This procedure contains two tasks. One task removes the reservoir fill indicator for the hydraulic systems. The other task installs the reservoir fill indicator for the hydraulic systems.
TASK 29-18-03-024-001
2. Remove the Reservoir Fill Indicator
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