(b)  
Remove the aft quadrant lockout tool.

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757 MAINTENANCE MANUAL
 H. Install the Reaction Link (Fig. 201)
 S 432-036
 (1)  
Do these steps to install the reaction link (3) on the trunnion block (19):

 (a)  
Install the end cap (33) on the top side (when installed on the airplane) of the trunnion block (19).

 (b)  
Put the reaction link (3) on the trunnion block (19) and do this step: 1) Install the pin (34), bolt (30), washer (31), and the nut

 (32)
 that connect the reaction link to the end cap. Tighten the nut to 145-165 pound-inches (16.4-18.6 newton-meters).

 (c)  
Lubricate the PCA and reaction link grease fittings after installation.

 S 422-037
 (2)  
Do these steps to install the actuator, reaction link, and trunnion block assembly:

 (a)  
Align the trunnion block (19), actuator (12), and reaction link (3) assembly with the airplane connection points.

 (b)  
Install the bolt (27), washer (28), and the nut (29) that connect the hanger link (26) to the trunnion block (19). Tighten the nut to 60 - 95 pound-inches (6.8-10.7 newton-meters).

 (c)  
Turn the actuator (12) and the reaction link (3) until they are aligned with the rudder front spar (4).

 (d)  
Install the bolts (5), washers (7), bushings (6), and nuts (8) that connect the actuator and the reaction link to the rudder front spar. Do these checks: 1) Make sure the torque that is necessary to turn the nut

 before it touches the spar is 90 - 400 pound-inches (10.2-45.1 newton-meters). 2) Tighten the nut to 1000 - 1400 pound-inches (113-158 newton-meters).
 S 432-038
 (3)  
Connect these components:

 (a)  
The input rod between the actuator shear out lever (17) and the torque tube (1)

 (b)  
The electrical connector for the rudder PCA monitor sensor

 (c)  
The hydraulic lines (2) to the actuator (12).

 S 862-039
 (4)  Move the rudder pedals to their full right position and hold them there.
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MAINTENANCE MANUAL

 S 862-075
 WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN
_______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
 (5)  Supply hydraulic pressure to the PCA that has the lockout tool installed (Ref 29-11-00).
 NOTE: The right system supplies the top PCA.
____
 The left system supplies the middle PCA.
 The center system supplies the bottom PCA.

 S 862-040
 (6)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:

 (a)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 (b)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (c)  
11H28, FLT CONT SHUTOFF TAIL RIGHT

 (d)  
11J10, PCU MON SENSOR

 (e)  
11J11, PCU MON MOD

 S 862-041
 (7)  
Remove the DO-NOT-OPERATE tags and move the FLT CONTROL SHUTOFF switches L, C, and R on the P61 panel to ON.

 S 862-043

 (8)  
Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00).

 S 092-042
 WARNING: DO NOT REMOVE THE PCA LOCKOUT TOOL WITH HYDRAULIC POWER ON.
_______ THE RUDDER CAN MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (9)  
Do these steps immediately after hydraulic power is removed:

 (a)  
Remove the PCA lockout tool.