S 424-012

 (2)  
Install the SMC on the E1-1 shelf and tighten the knob (AMM 20-10-07/201).

 NOTE: Be careful not to cause damage to the electrical connectors
____
 on the back of the SMC.

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 D. SMC Test
 S 864-011
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 864-010

 (2)
Open SMC STALL WARN ASYM MODE circuit breaker on the P18-2 panel.

 S 864-001

 (3)  
Prepare for the pitch limit check:

 (a)  
Set the IRS L and IRS R mode selector switches (aft P-5 overhead panel) to the NAV position.

 (b)  
Set the IRS transfer switch (forward P-5 overhead panel) to the NORMAL position.

 (c)  
Set the EFI transfer switch (forward P-5 overhead panel) to the NORMAL position.

 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL
_______ CONTROL SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATOR, FLAPS SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (d)  Set the HYD PUMP B ELEC 1 switch (P5 overhead panel ) to the ON position (AMM 27-81-00/201).
 S 864-002
 (4)  
If you replaced SMC 1, close these circuit breakers:

 (a)  
P18-2 Panel
 1) SMC 1 CMPTR DC
 2) SMC 1 SNSR EXC AC

 (b)  
P6-2 Panel
 1) AUTOSLAT 1 DC

 S 864-003
 (5)  
If you replaced SMC 2, close these circuit breakers:

 (a)  
P6-1 Panel
 1) SMC 2 CMPTR DC
 2) SMC 2 SNSR EXC AC

 (b)  
P6-2 Panel
 1) AUTOSLAT 2 DC

 S 744-004
 (6)  
Do a BITE test of the stall warning system:

 (a)  
Push the ON/OFF button on the SMC maintenance control panel on the front of the SMC.

 (b)  
Make sure that the display on the SMC shows TEST IN PROGRESS and then shows SYSTEM OK.

 (c)  
Push the ON/OFF button.

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737-300/400/500MAINTENANCE MANUAL
 (d)  Make sure that the display shows EXITING BITE and then is blank.
 S 714-005
 (7)  Do an operational test of the applicable stall warning system: (a) Push and hold the STALL WARNING TEST NO. 1 switch (for SMC 1) or NO. 2 switch (for SMC 2) on the stall warning test module (P5 overhead panel). (b) Make sure that the captain's (for SMC 1) or first officer's (for SMC 2) control column shaker operates. (c) Release the switch. (d) Make sure that the control column shaker stops.
 S 714-006
 (8)  Make sure that a pitch limit symbol shows on the captain's and first officer's EADI's after you move the flap lever to the one unit position.
 S 864-022
 (9)  Return the flap lever to the zero unit position.
 S 864-021

 (10)
 Set the HYD PUMP B ELEC 1 switch (P5 overhead panel) to OFF (AMM 27-81-00/201).

 S 864-007

 (11)
 Set the IRS L and IRS R mode selector switches to the OFF position.

 S 864-008

 (12)
 Close SMC STALL WARN ASYM MODE circuit breaker on the P18-2 panel.

 S 864-009

 (13)
 Remove electrical power (AMM 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
　
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