B.
References

 (1)  
AMM 06-09-05/201, Body Section 48 Access Doors and Panels

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (4)  
AIPC 27-48-52, Fig. 1

 (5)  
SSM 27-48-01

 (6)  
WDM 27-48-11

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A
747-400
MAINTENANCE MANUAL

 C. Access
 (1)  
Location Zone
 315, 316 Area Aft of Stabilizer Box

 (2)  
Access Panel
 315A Access Door

 D.
Install the Transmitter Module

 S 144-010
 (1)  
Clean the sealant from the mounting bracket.

 S 424-011

 (2)  
Install the transmitter module on the bracket so that splined shaft engages with crank.

 S 434-012

 (3)  
Install three screws, washers, and nuts.

 (a)  
Tighten the nuts.

 S 434-013
 (4)  
Install the electrical connector.

 E.
Adjust the Transmitter module

 S 864-014
 (1)  
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).

 S 864-016

 (2)  
Do this task: "Supply Hydraulic Power" (AMM 29-11-00/201).

 S 864-017

 (3)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P7, Overhead Circuit Breaker Panel
 1) 7E23, STAB TRIM ALTN CONT
 2) 7E20, STAB TRIM R S/O VALVE

 (4)  
Set the STAB TRIM 3 switch to ON.

 S 864-018
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-019
 WARNING:_______ MOVE ALL PERSONS AND EQUIPMENT AWAY FROM THE STABILIZER AND
 THE ELEVATOR SURFACES BEFORE YOU MOVE THE STABILIZER.  THE
 STABILIZER AND THE ELEVATOR SURFACES CAN MOVE QUICKLY AND CAUSE

 INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (5)  Use the STAB TRIM ALTN switches to move the stabilizer until the "B" dimension is 17.59-17.63 inches (446.8-447.8 millimeters).
 NOTE: The "B" dimension is the distance along the ballscrew between
____ the surfaces of the ballnut and the ballscrew stops
 S 864-020
 (6)  
Set the STAB TRIM 3 switch to CUTOUT.

 S 864-021

 (7)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P7, Overhead Circuit Breaker Panel 1) 7E20, STAB TRIM R S/O VALVE 2) 7E23, STAB TRIM ALTN CONT

 S 864-022
 (8)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6, Main Power Distribution Panel 1) 6K23, STAB TRIM POSN IND L 2) 6K24, STAB TRIM POSN IND R

 (b)  
P7, Overhead Circuit Breaker Panel 1) 7C10, FLT CONT ELEC 2L AC 2) 7C11, FLT CONT ELEC 2L DC 3) 7C12, FLT CONT ELEC 1L AC 4) 7C13, FLT CONT ELEC 1L DC

 S 864-023
 (9)  
If the hydraulic power is not necessary, do this task: "Remove Hydraulic Power" (AMM 29-11-00/201).

 S 834-024

 (10)
 Adjust the transmitter control rod:

 (a)  
Loosen the jamnut at the two ends of the applicable transmitter control rod.

 (b)  
Adjust the control rod until the applicable indication on the EICAS flight controls maintenance page shows 4.49-4.51 degrees down.

 (c)  
Tighten the jamnut at the two ends of the control rod.

 (d)  
Make sure the EICAS indication is still in the tolerance.

 (11)
 Seal the joint and the two ends of the fastener with sealant.
　
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