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____ warning system No. 1 and the left transmitter supplies system No. 2.
 NOTE: It is possible that the aural warning horn will energize
____ at the flaps 25 position.
 (b)  
Turn the right AOA sensor clockwise slowly until the first officer's control column shaker operates.

 (c)  
Make sure that the shaker started to operate at the applicable point in Table 501.

 (d)  
Turn the right AOA sensor counterclockwise to the zero position.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DIGITAL STALL WARNING ú

 27-32-00
 COMPUTER P/N 65-52819  ú CONFIG 1 ú 01 Page 506 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~.............................................................................. | Table 501 | ................................................................................ | FLAP | AOA SENSOR POSITION FOR SHAKER OPERATION *[1] | | POSITION | (tolerance |1.0° or |60 minutes) | ................................................................................ | | *[2] | *[3] | | 0 | 2.0° (2° 0')| +(-) aerodynamic offset | ................................................................................ | 1 | 9.2° (9°12')| +(-) aerodynamic offset | ................................................................................ | 2 | 8.9° (8°54')| +(-) aerodynamic offset | ................................................................................ | 5 | 8.8° (8°48')| +(-) aerodynamic offset | ................................................................................ | 10 | 8.5° (8°30')| +(-) aerodynamic offset | ................................................................................ | 15 | 8.0° (8° 0')| +(-) aerodynamic offset | ................................................................................ | 25 | 7.6° (7°36')| +(-) aerodynamic offset | ................................................................................ | 30 | 7.0° (7° 0')| +(-) aerodynamic offset | ................................................................................ | 40 | 6.0° (6° 0')| +(-) aerodynamic offset | 2.....................…....................…...................................1
 *[1] Turn the left AOA sensor counterclockwise and add theaerodynamic offset.
 Turn the right AOA sensor clockwise and subtract the aerodynamic offset. *[2] 0.1° = 0° 6' *[3] The aerodynamic offset in degrees shows on the trailing edge of the
 AOA sensor.
 S 865-015-001
 (12)
 Move the flap control lever to the UP position and let the flaps retract.

 S 865-016-001

 (13)
 Open this circuit breaker:

 (a)  
P6 Panel
 1) STALL WARN DC

 

 S 865-017-001
 (14)
 Close this circuit breaker:

 (a)  
P18 Panel
 1) STALL WARN DC

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH DIGITAL STALL WARNING ú

 27-32-00
 COMPUTER P/N 65-52819  ú  CONFIG  1
 ú  01  Page 507
 ú  Mar 15/99 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 715-018-001
 (15)
 Make sure that the left AOA sensor controls the captain's control column shaker:

 (a)  
Turn the left AOA sensor slowly counterclockwise (trailing edge up) until the captain's control column shaker operates.

 (b)  
Turn the sensor 10° farther than the point where the shaker started to operate.

 (c)  
Make sure that the shaker continues to operate.

 (d)  
Turn the left AOA sensor clockwise (trailing edge down) to the range where the shaker does not shake.

 S 715-019-001
 (16)
 Make sure that the stall warning system No. 1 operates correctly at each flap position given in Table 501:

 (a)  
Move the flap control lever to the applicable position in Table 501 and let the flaps extend.

 (b)  
　
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