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A 737-300/400/500MAINTENANCE MANUAL
 S 075-082-001
 (4)  Erase the stall warning computer No. 1 fault memory: (a) Push and hold the START BITE switch on the front of stall warning computer No. 1. (b) When one or more light starts to flash after 10 to 20 seconds, release the START BITE switch. The memory is now clear.
 S 075-083-001
 (5)  Erase the stall warning computer No. 2 fault memory: (a) Push and hold the START BITE switch on the front of stall warning computer No. 2. (b) When one or more light starts to flash after 10 to 20 seconds, release the START BITE switch. The memory is now clear.
 S 865-088-001
 (6)  Remove the system B hydraulic power (Ref 27-81-00/201).
 S 865-098-001
 (7)  Close these circuit breakers: (a) P6 Panel 1) AUTOSLAT 1 AC 2) AUTOSLAT NO. 1 DC 3) AUTOSLAT 2 AC 4) AUTOSLAT NO. 2 DC 5) LANDING GEAR AIR/GND RELAY AND LTS (b) P18 Panel 1) STALL WARN ASYM MODE
 S 865-009-001
 (8)  Remove the DO-NOT-CLOSE tags and close these circuit breakers: (a) P18 Panel 1) L ALPHA VANE HTR 2) R ALPHA VANE HTR
 S 865-090-001
 (9)  Remove electrical power (Ref 24-22-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DIGITAL STALL WARNING ú

 27-32-00
 COMPUTER P/N 65-52819  ú CONFIG 1 ú 01 Page 518 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 STALL WARNING SYSTEM - ADJUSTMENT/TEST
______________________________________
 1.  General_______
 A.  This subject contains two tasks. The first task is an operational test of the stall warning system. You will do the operational test in the control cabin.
 B.  The second task is a system test. The system test has these parts:
 -Stall Warning Operational Test (Confidence Test)
 -
SMC Discrete Inputs Test

 -
SMC ARINC Inputs Test

 -
SMC 1 AOA Sensor Input Test

 -
SMC 2 AOA Sensor Input Test

 -
SMC Flap Position Inputs Test

 -
SMC Engine Tachometer Inputs Test

 -
SMC to EFIS Interface Test

 -
SMC Asymmetry Mode Test

 C.  
You will use the buttons on the front of the stall management computers (SMC) to do a BITE test and to monitor the inputs to the SMC's.

 D.  
In the system test, you will open and close circuit breakers in the control cabin, push buttons on the E-11 landing gear logic shelf, manually change the position of the AOA sensors, and extend and retract the flaps.

 E.  
In the Engine Tachometer Inputs Test you will connect a stall warning system test box at the engine tachometer transmitters inside the engine cowls. As an alternative method to do this test, you can connect a dc power supply at the engine tachometer indicators in the flight compartment.

 TASK 27-32-00-715-053-002
 2.  Operational Test - Stall Warning System_______________________________________
 A.  References
 (1)
24-22-00/201, Manual Control

 B.  
Access

 (1)  
Location Zone
 101, 102 Control Cabin

 C.  
Procedure

 (1)
Supply electrical power (Ref 24-22-00/201).

 S 865-063-002
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú

 27-32-00
 COMPUTER P/N 65-52822  ú CONFIG 2 ú 02 Page 501 ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 715-064-002
 (2)  
Do an operational test of the No. 1 stall warning system:

 (a)  
Push and hold the STALL WARNING TEST NO. 1 switch on the stall warning test module (P5-18 overhead panel).

 (b)  
Make sure that the captain's control column shaker operates both columns.

 (c)  
Release the switch.

 (d)  
Make sure that the shaker stops.

 S 715-065-002
 (3)  
Do an operational test of the No. 2 stall warning system:
　
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