C. DFCS Flight Mode Annunciator
 S 424-001
 (1)  Install the FMA:
 (a)  
Connect the electrical connectors at the rear of the FMA.

 (b)  
Push the FMA in its position.

 (c)  
Install the mounting screws.

 S 864-002
 (2)  Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a)  
P6 Circuit Breaker Panel
 1) AFCS B MACH TRIM DC
 2) AFCS B MACH TRIM AC
 3) AFDS MCP CRS-2
 4) AFCS B SNSR EXC AC
 5) AFCS B FCC DC
 6) AFCS B ENGAGE INTLK
 7) AFCS B WARN LIGHT BAT

 (b)  
P18 Circuit Breaker Panel
 1) AUTOTHROTTLE AC
 2) AUTOTHROTTLE DC
 3) AFDS MCP DC

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A
737-300/400/500MAINTENANCE MANUAL
 4) Airplanes with mechanical aileron force limiter:
 AFCS AIL FORCE LIM
 5) AFCS A SNSR EXC AC
 6) AFCS A FCC DC
 7) AFCS A ENGAGE INTLK
 8) AFCS A WARN LIGHT BAT
 9) AFCS A MACH TRIM AC
 10) AFCS A MACH TRIM DC
 11) FMCS CDU NO. 1
 12) FMCS CDU NO. 2
 13) MODE ANN
 14) FMCS CMPTR

 S 714-003
 (3) Do this task: "DFCS Annunciator" (AMM 22-11-35/501).
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737-300/400/500MAINTENANCE MANUAL
 DFCS ANNUNCIATOR - ADJUSTMENT/TEST
__________________________________
 1.  General
_______
 A.  This procedure contains the installation test of the DFCS Flight Mode Annunciator (FMA).
 B.  The DFCS Built-In Test Equipment (BITE) is used to do the operational test after the installation of the DFCS Flight Mode Annunciator (FMA). This test makes sure that the FMA operates correctly. It uses no external equipment. The airplane electrical and hydraulic systems are the only power sources necessary for this task.
 TASK 22-11-35-745-001
 2.  DFCS Flight Mode Annunciator BITE Test
______________________________________
 A.  References
 (1)  
22-11-00/501, Digital Flight Control System

 (2)  
24-22-00/201, Manual Control

 B.  Access
 (1)  Location Zones
 101 Control Cabin, Left
 102 Control Cabin, Right

 C.  DFCS Flight Mode Annunciator BITE Test
 S 745-003
 (1)  
Do the preparation for the DFCS BITE test in this task: "Operational Test - Digital Flight Control System" (Ref 22-11-00/501).

 S 745-002

 (2)  
Do the FMA interface test:

 (a)  
Push the INIT REF key on the CDU keyboard.

 (b)  
Push the line-select key (LSK) adjacent to <MAINT.

 (c)  
Push the LSK adjacent to <DFCS.

 (d)  
Push the LSK adjacent to <LRU INTERFACE.

 (e)  
Push the LSK adjacent to <CHANNEL A or <CHANNEL B.

 (f)  
Push the NEXT PAGE key on the CDU keyboard.

 (g)  
Push the LSK adjacent to <FMA.

 (h)  
Do the preparation steps as shown on the CDU display.

 (i)  
Follow the CDU instructions and push the LSK adjacent to <CONTINUE until the test is completed with no failure.

 (j)  
If a failure occurs, do these steps: 1) From the CDU display, make a note of the channel and the

 LRU that caused the failure. 2) Replace the defective component.
 NOTE: Before you replace a defective component, do the
　
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