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757 MAINTENANCE MANUAL
 (4)  S 434-028On the inboard PCA linkage only, connect the PCA input rod to the crank assembly (View B).
 (5)  S 434-029Connect the two ends of the pogo rod.
 NOTE:____ If you changed the adjustment of the pogo rod while it was disconnected, do the elevator PCA adjustment (Ref 27-31-00).
 (6)  S 434-030On the center and outboard PCA linkages only, connect the centering spring to the crank assembly (View C and D).
 (7)  S 094-031Remove the PCA lock assembly (Fig. 402).
 (8)  S 094-032Remove the rope and DO-NOT-OPERATE tags from the control columns and let the control columns go to the neutral position.
 (9)  S 864-033Remove the DO-NOT-CLOSE tags and close these circuit breakers on the overhead panel, P11: (a) 11B19, STAB TRIM ALT (IF INSTALLED) (b) 11C12, STAB TRIM SHUTOFF LEFT (c) 11C13, STAB TRIM SHUTOFF RIGHT (d) 11H11 or 11C05, STAB TRIM CONT L (e) 11H17, FLT CONT SHUTOFF TAIL LEFT (f) 11H18, FLT CONT SHUTOFF TAIL CTR (g) 11H20, STAB TRIM CONT R (h) 11H28, FLT CONT SHUTOFF TAIL RIGHT (i) 11J10, PCU MON SENSOR

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757 MAINTENANCE MANUAL
 (j)  11J11, PCU MON MOD
 S 864-034
 (10)
 Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the NORM position.

 S 864-035

 (11)
 Put the L, R, and C FLT CONTROL SHUTOFF switches on the right side panel, P61, to the ON position.

 S 824-036

 (12)
 Do the adjustment for the elevator PCAs (Ref 27-31-00).

 S 714-037

 (13)
 Do the test for the elevator travel limits (Ref 27-31-00).

 E.
Put the Airplane Back to Its Usual Condition

 S 444-038
 (1)  
Do the activation procedure for the spoilers if it is necessary (Ref 27-61-00).

 S 434-039

 (2)  
Install the trailing edge beam and seal panel.

 S 414-040

 (3)  
Install the access panel for the elevator PCAs, 335DB (left elevator PCAs) or 345DB (right elevator PCAs) (Ref 06-42-00).

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757 MAINTENANCE MANUAL
 CONTROL COLUMN - REMOVAL/INSTALLATION
_____________________________________
 1.  General_______
 A.  The removal/installation procedures for the captain's and first officer's control columns are the same.
 TASK 27-31-10-024-001
 2.  Remove the Control Column_________________________
 A.  Equipment
 (1)  
Extraction/Insertion Tool - M15570-20
 Deutsch Company, Electronic Components Division
 700 S. Hathaway, Municipal Airport
 Banning, CA 92220

 (2)  
Rig Pin E/ST6 -P/N B20003-21, part of Set B20003-XX (Ref 20-10-24)

 B.  
References

 (1)  
06-41-00/201, Fuselage Access Doors and Panels

 (2)  
20-10-24/201, Rig Pins

 (3)  
24-22-00/201, Electrical Power - Control

 (4)  
SWPM 20-61-16, Standard Wiring Practices Manual

 C.  
Access

 (1)  
Location Zones 113 Area Forward of NLG Wheel Well (Left) 211/212 Control Cabin

 (2)  
Access Panel
 113AL Forward Compartment Access Door

 D.  
Prepare for the Removal

 S 864-002
 (1)  
Supply electrical power (Ref 24-22-00).

 S 214-004

 (2)  
Make sure that the control column is at neutral.

 S 864-005

 (3)  
Put the R, L, and C FLT CONTROL SHUTOFF switches on the sidewall panel, P61, to OFF.
　
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