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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 864-035
 (17)
 Make sure the cable tension is in the limits (Fig. 402).

 S 864-036

 (18)
 Set the stabilizer B dimension to 41.57 +0.01/-0.00 inches (Fig. 402).

 S 824-037

 (19)
 Turn the flexible shaft until the stabilizer trim indicators align with 3.00 | 0.25 stabilizer trim units.

 S 434-038

 (20)
 Install the flexible shaft in the drum shaft in the forward mechanism.

 (a)  
Make sure the splines engage before you tighten the union.

 S 434-039
 (21) Install the drip shield (not on all airplanes) on the bottom of the gear housing.
 S 864-051
 CAUTION: IF YOU DO NOT KEEP SUFFICIENT CLEARANCE, WIRES CAN BE DAMAGED.
_______
 (22)
 Make sure that the clearance between the chain and the adjacent wire bundle is as follows:

 (a)  
The lateral clearance must be not less than 0.5 inch.

 (b)  
The vertical clearance (measured parallel to the chain) must be not less than 1.5 inches.

 (23)
 Close the access door 1103.

 S 864-042

 (24)
 If the electrical power is not necessary, remove the electrical power (AMM 24-22-00/201).

 S 414-034
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 COLUMN CUTOUT SWITCH - REMOVAL/INSTALLATION
___________________________________________
 1.  General_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the column cutout switch. The procedure has these parts:
 (1)  
The removal of the column cutout switch

 (2)  
The installation of the column cutout switch

 TASK 27-41-51-004-001
 2.  Column Cutout Switch Removal (Fig. 401)____________________________
 A.  Access
 (1)  
Location Zones
 101 Control Cabin, LH
 102 Control Cabin, RH
 202 Lower Nose Compartment

 (2)  
Access Panels
 1103 Forward Access Door

 B.  
Procedure

 S 864-003
 (1)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6-2 Circuit Breaker Panel
 1) STABILIZER TRIM CONT
 2) STABILIZER TRIM ACTUATOR

 S 014-002
 (2)  
Open the access door 1103.

 S 024-004

 (3)  
Remove the column cutout switch:

 (a)  
Disconnect the rod assembly (1) from the switch arm (2).

 (b)  
Disconnect the electrical connectors.

 (c)  
Remove the mounting bolts (3).

 TASK 27-41-51-404-005
 3.  Column Cutout Switch Installation (Fig. 401)_________________________________
 A.  Special Tools and Equipment
 (1) Rig Pin ST-4 - 0.182/0.186-inch diameter, 3.50 | 0.25 inches long
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 ALL  ú ú 01 Page 401 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

RIG PIN HOLE

Column Actuated Cutout Switch
Figure 401

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