NOTE: If the voltage decreases, the adjustment is correct.
____
 (g)  
Do the adjustment again if the voltage does not decrease.

 (h)  
Install the lockwire on the thumb nut (on the microadjustment rod) when the adjustment is correct.

 S 415-014
 (3)  
Connect the sensor connectors:

 (a)  
Disconnect the VTVM.

 (b)  
Remove the test cable.

 (c)  
Connect the sensor connectors.

 (d)  
Remove the test set cable.

 (e)  
Connect the D1681 connector to the A/P actuator A.

 (f)  
Connect the D1687 connector to the A/P actuator B.

 (g)  
Remove the power cable of the test set.

 (4)  
Close these circuit breakers and remove the DO-NOT-CLOSE tags:

 S 865-015
 NOTE: Make sure that you close the AFCS A FCC DC And AFCS B FCC DC
____
 circuit breakers last.

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 22-11-14
 ALL  ú ú 01 Page 505 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (a)  
P6 Circuit Breaker Panel 1) AUTO FLT CONT SYS B MACH TRIM AC 2) AUTO FLT CONT SYS B MACH TRIM DC 3) AFDS MCP CRS-2 4) AUTO FLT CONT SYS B SNSR EXC AC 5) AUTO FLT CONT SYS B FCC DC 6) AUTO FLT CONT SYS B ENGAGE INTLK B 7) AUTO FLT CONT SYS B WARN LIGHT BAT

 (b)  
P18 Circuit Breaker Panel 1) AUTO FLT CONT SYS A MACH TRIM AC 2) AUTO FLT CONT SYS A MACH TRIM DC 3) AFDS MCP DC 4) ALL EXCEPT AIRPLANES WITH -914 AND ON FCC;

 AFDS AIL FORCE LIM 5) AUTO FLT CONT SYS A SNSR EXC AC 6) AUTO FLT CONT SYS A FCC DC 7) AUTO FLT CONT SYS A ENGAGE INTLK A 8) AUTO FLT CONT SYS A WARN LIGHT BAT
 S 415-016
 (5)  Install the 3802 access door on the tail cone.
 H. Sensor Adjustment Check
 S 745-018
 (1)  Do the Pitch Sensor Check (tests 51.01 through 51.05) in this task: "Rigging Test" (Ref 22-11-01/501 or 22-11-00/501).
 NOTE: This task uses the BITE to do the sensor adjustment
____
 check.

 TASK 22-11-14-825-035
 3. Elevator Neutral Shift Sensor Adjustment (DFCS BITE) (-912 and on)
________________________________________
 A. General
 (1)  In this procedure, you use the DFCS BITE to do the adjustment. This adjustment procedure is part of the DFCS BITE. To do the adjustment, you have to remove the 3802 access door to get access to the sensor.
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 22-11-14
 ALL  ú ú 05 Page 506 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 B.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
You can find the sensor on the forward right side of the feel and centering unit. The feel and centering unit is aft of the bulkhead station 1156.

References

 (1)  
12-31-41/201, Body Section 48 Access Doors and Panels

 (2)  
22-11-00/501 or 22-11-01/501, Digital Flight Control System

 (3)  
27-31-00/501, Elevator and Tab Control System

 (4)
27-41-81/401, Stabilizer Ball Nut and Jackscrew GearboxAccess

 (1)  
Location 705 Tail Cone

 (2)  
Access Panel

 3802 Tail Cone Access DoorPrepare for sensor adjustment
 S 865-038
 (1)  
Do this task to fully adjust the elevator rigging before you can adjust the neutral shift sensor: "Adjustment - Elevator and Tab Control System" (Ref 27-31-00/501).

 S 015-020

 (2)  
Remove the 3802 access door on the tail cone (Ref 12-31-41/201).

 S 745-034

 (3)  
Do the preparation for the DFCS BITE Test in this task: "Operational Test - Digital Flight Control System" (Ref 22-11-00/501 or 22-11-01/501).

Sensor Adjustment
 S 745-023
 (1)  Get access to the OVERNIGHT MAINT 2/2 page:
 (a)  
　
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