S 865-116

 (21)
 Close the TR2 circuit breakers on the P6-4 Circuit Breaker Panel.

 S 865-117

 (22)
 Set the meter selector switch for the TRU to the TR1 position.

 S 215-141

 (23)
 Make sure the TRU meter on the pilot's overhead panel is 22 to 30v dc.

 S 865-183

 (24)
 Open the TR1 circuit breakers on the P6-4 Circuit Breaker Panel.

 S 865-119

 (25)
 Open the AFCS A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.

 S 745-191

 (26)
 Make sure that the DC voltmeter on the Pilots' Overhead Panel, P5-13 reads 22 to 30v dc.

 S 745-120

 (27)
 Do the steps (5) thru (11) until the CDU display shows the CHANNEL SELECTION page.

 S 745-121

 (28)
 Push the LSK adjacent to <CHANNEL B to show the FCC memory contents of channel B.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 22-11-01
 ú ú 24 Page 571 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 745-122
 (29)
 Push the LSK adjacent to <TEST SELECTION.

 S 745-123

 (30)
 Use the CDU keyboard to put the library test No. 13 on the screen and in the memory.

 S 745-124

 (31)
 Push the LSK 6R to put the library test No. 13 on the screen and in the memory.

 S 745-125

 (32)
 Push the LSK adjacent to <EXECUTE to do the test 60.13 (MCP Interface Quick Test).

 S 745-126

 (33)
 Do the preparation steps as shown on the CDU display but keep the TR1, TR3, and AFCS A FCC DC circuit breakers open.

 S 745-127

 (34)
 Push the LSK adjacent to <CONTINUE until the question "DFCS BITE INOP and CHECK FCC or INTERFACES are normal ?

 S 745-128

 (35)
 Make sure that the DC voltmeter on the Pilots' Overhead Panel, P5-13 is at 0v dc when the question "Is the word TEST displayed on the F/O EADI?" is shown on the CDU.

 S 865-129

 (36)
 Close the TR1 and TR3 circuit breakers on the P6-4 Circuit Breaker Panel.

 S 865-130

 (37)
 Close the AFCS A FCC DC circuit breaker on the P18-1 Circuit Breaker Panel.

 (38)
 Push the INIT/REF key on the CDU keyboard to get out of the BITE.

 S 745-160
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú

 22-11-01
 ú ú 06 Page 572 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ROLL CONTROL WHEEL STEERING FORCE TRANSDUCER -
______________________________________________ REMOVAL/INSTALLATION
____________________
 1.  General (Fig. 401)_______
 A.  This procedure contains two tasks. The first task is for the removal of the roll force transducer. The second task is for the installation of the roll force transducer.
 B.  You can find the roll force transducer on the aileron drum at the bottom of the captain's column.
 TASK 22-11-11-004-025
 2.  Roll Force Transducer Removal_____________________________
 A.  References
 (1)  12-31-11/201, Body Section 41 Access Doors and Panels
 B.  Access
 (1)  
Location Zone
 202 Lower Nose Compartment

 (2)  
Access Panel
 1103 Forward Access Doors

 C.  Procedure
 S 864-026
 (1) Open these circuit breakers and attach the DO-NOT-CLOSE tags:
 (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

　
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