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Stall Warning Test Module Installation
Figure 401/27-32-21-990-801
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TASK 27-32-21-400-801
3. Stall Warning Test Module Installation
(Figure 401)
A. References
Reference Title
24-22-00-860-813 Supply External Power (P/B 201)
24-22-00-860-814 Remove External Power (P/B 201)
B. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Stall warning test module 27-32-21-01-005 GUN 101-110, 156, 157
C. Stall Warning Test Module Installation
SUBTASK 27-32-21-420-001
(1) Connect the electrical connectors to the stall warning test module [1].
SUBTASK 27-32-21-420-002
(2) Install the stall warning test module [1] in the aft overhead panel.
SUBTASK 27-32-21-410-001
(3) Tighten the fasteners.
SUBTASK 27-32-21-860-002
(4) Remove the safety tags and close these circuit breakers:
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 5 C01204 SMYD-1 CMPTR DC
F/O Electrical System Panel, P6-1
Row Col Number Name
B 5 C01206 SMYD-2 CMPTR DC
D. Stall Warning Test Module Installation Test
SUBTASK 27-32-21-860-003
(1) Do this task: Supply External Power, TASK 24-22-00-860-813.
SUBTASK 27-32-21-860-004
(2) Push and hold the STALL WARNING TEST NO. 1 switch on the module.
NOTE: The amber SPD LIM light on the on-side Primary Flight Display will come on. A YAW
DAMPER light on the P5-3 panel with a related MASTER CAUTION light is possible. A
SPD LIM annunciation that stays on more than 5 seconds after the stick shaker
operates could be a problem.
(a) Make sure that the captain’s control column shaker operates.
SUBTASK 27-32-21-860-005
(3) Release the STALL WARNING TEST NO. 1 switch.
(a) Make sure that the shaker stops.
SUBTASK 27-32-21-860-006
(4) Push and hold the STALL WARNING TEST NO. 2 switch on the module.
(a) Make sure that the first officer’s control column shaker operates.
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SUBTASK 27-32-21-860-007
(5) Release the STALL WARNING TEST NO. 2 switch.
(a) Make sure that the shaker stops.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-32-21-210-004
(1) If electrical power is not necessary, do this task: Remove External Power,
TASK 24-22-00-860-814.
------------------------- END OF TASK ---------------------------
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CONTROL COLUMN SHAKER - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) Removal of the control column shaker.
(2) Installation of the control column shaker.
TASK 27-32-31-000-801
2. Control Column Shaker Removal
(Figure 401)
A. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
B. Prepare for the Removal
SUBTASK 27-32-31-860-001
(1) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 4 C01392 STICK SHAKER LEFT
F/O Electrical System Panel, P6-1
Row Col Number Name
B 6 C01393 STICK SHAKER RIGHT
C. Shaker Removal
SUBTASK 27-32-31-020-001
(1) Disconnect the electrical connector from the shaker [1].
SUBTASK 27-32-31-020-002
(2) Remove the nuts [4], bolts [5], shims [3], and spacers [2] which attach the shaker [1] to the strap
on the control column.
SUBTASK 27-32-31-020-003
(3) Remove the shaker [1] from the control column.
------------------------- END OF TASK ---------------------------
TASK 27-32-31-400-801
3. Control Column Shaker Installation
(Figure 401)
A. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Shaker 27-32-31-01-035 GUN 001-026, 101-120,
155-157, 201-999
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(103)
