(b)  
P7, Overhead Circuit Breaker Panel
 1) 7D7, FLT CONT CMPTR SERVO L
 2) 7D8, FLT CONT CMPTR PWR L
 3) 7D12, FLT CONT CMPTR SERVO C
 4) 7D14, FLT CONT CMPTR SERVO R
 5) 7D15, FLT CONT CMPTR PWR R

 S 012-061
 (2)  Make sure that you remove the access panels 324EL, 324FL, and 324FR (optional)(AMM 06-09-07/201).
 E.  Rollout Power Control Package and Override Mechanism Adjustment
 S 832-062
 (1)  Put the rig pin through the centering unit bellcrank and the channel on the structure.
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 S 832-063
 (2)  
Put the rig pin through the control rod assembly and the RPCP mounting base.

 S 832-064

 (3)  
If the rig pin does not go through easily, adjust the length of the clevis/tube assembly.

 (a)  Do these steps for the fine adjustment: 1) Loosen the checknuts. 2) Turn the sleeve a maximum of two turns until you can put
 the rig pin through the hole. Tighten the check nuts.
 NOTE: A maximum length of 1.15 inches is permitted between
____ the sleeve and the tube.
 (b)  If the fine adjustment is not sufficient, do these steps for the coarse adjustment: 1) Loosen the checknuts. 2) Remove the bonded-bolt assembly through the clevis and the
 override mechanism. 3) Turn the clevis assembly a maximum of two turns until you can put the rig pin through the hole.
 NOTE: One completed turn changes the length of the
____ assembly 0.042 inches. A maximum length of 1.52 inches is permitted between the clevis thread and the tube.
 4) Connect the clevis to the override mechanism.
 CAUTION: DO NOT TIGHTEN THE LARGE NUT AGAIN AFTER YOU TIGHTEN
_______ THE SMALL NUT. DAMAGE TO THE BONDED-BOLT ASSEMBLY CAN OCCUR.
 (c)  Tighten the large nut to 60-80 pound-inches and the small nut to 30-40 pound-inches. 1) Do the fine adjustment if it is necessary.
 S 012-065
 (4)  
Remove the rig pins.

 S 832-066

 (5)  
Visually examine the RPCP and the override mechanism to make sure that the adjustment is satisfactory.

 TASK 22-13-04-702-067
 7. Rollout Power Control Package Test
__________________________________
 A. References
 (1)  
AMM 21-58-00/501, Electrical/Electronic Equipment Cooling System

 (2)  
AMM 22-10-00/501, Autopilot/Flight Director System

 (3)  
AMM 24-22-00/201, Manual Control

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 (4)  AMM 29-11-00/201, Main Hydraulic Supply System
 B. Access
 (1)  Location Zones
 221 Control Cabin, LH
 222 Control Cabin, RH

 C. Prepare for the Rollout Power Control Package Test
 S 862-070
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 862-071

 (2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6, Main Power Distribution Panel
 1) 6J24, RUD/ELEV SENSOR
 2) 6J25, RUD/ELEV IND

 (b)  
P7, Overhead Circuit Breaker Panel
 1) 7D7, FLT CONT CMPTR SERVO L
 2) 7D8, FLT CONT CMPTR PWR L
 3) 7D12, FLT CONT CMPTR SERVO C
 4) 7D13, FLT CONT CMPTR PWR C
 5) 7D14, FLT CONT CMPTR SERVO R
 6) 7D15, FLT CONT CMPTR PWR R
 7) 7D16, RUD TRIM CONT

 S 862-091
 (3)  Set the FLT CONTROL HYD POWER TAIL 1, 2, 3, and 4 switches to the NORM position. These switches are on the Pilots' Overhead Maintenance Panel, P461.
　
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