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F/O Electrical System Panel, P6-1
Row Col Number Name
B 4 C01207 SMYD-2 SNSR EXC AC
B 5 C01206 SMYD-2 CMPTR DC
B 6 C01393 STICK SHAKER RIGHT
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-32-42-740-001
(3) Push the NO. 1 STALL WARNING TEST switch.
(a) Make sure the captain’s shaker operates.
SUBTASK 27-32-42-740-002
(4) Push the NO. 2 STALL WARNING TEST switch.
(a) Make sure the first officer’s shaker operates.
SUBTASK 27-32-42-740-003
(5) Push the MASTER CAUTION switch.
(a) Make sure the AUTOSLAT FAIL light is off.
SUBTASK 27-32-42-740-004
(6) Do the SMYD EXISTING FAULTS test.
(a) Turn on the SMYD BITE by pushing the ON/OFF switch.
NOTE: EXISTING FAULT? should show.
(b) Push the YES switch.
(c) Make sure NO FAULTS shows on the display.
SUBTASK 27-32-42-740-005
(7) Do the SWEEP TEST on the SMYD. To do the test, do this task: Stall Management Yaw Damper
(SMYD) BITE Test - Ground Test, TASK 27-32-00-740-803.
NOTE: This test is part of the SERVO TEST which is part of the SMYD GROUND TEST.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-32-42-860-007
(1) Push the ON/OFF switch on the SMYD BITE panel to turn the SMYD BITE off.
SUBTASK 27-32-42-410-001
(2) Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
------------------------- END OF TASK ---------------------------
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EFFECTIVITY
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HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - ADJUSTMENT/TEST
1. General
A. This procedure has these tasks:
(1) Stabilizer Control Cable and Chain Adjustment - Use this task to adjust the horizontal stabilizer
control cables and chain.
(2) Stabilizer Manual Trim and Trim Indicator Test - Use this test to make sure the horizontal
stabilizer moves to the correct position when it is operated from the stabilizer trim wheel. This
test also makes sure that the stabilizer trim indicator operates correctly.
(3) Stabilizer Trim Control System Friction Test - Use this test to check the force to operate the
horizontal stabilizer.
(4) Stabilizer Electric Trim System Test - Use this test to make sure the horizontal stabilizer moves
at the correct speed when it is operated from the STAB TRIM switches.
(5) Stabilizer Trim Wheel Free Movement Test - Use this test to test the amount of horizontal
stabilizer movement after the STAB TRIM switches are released.
(6) Stabilizer Trim Limit Switches Test - Use this test to make sure the stabilizer trim limit switches
operate correctly.
(7) Stabilizer Clutch Friction System Test - Use this test to make sure that the correct force will
disconnect the manual clutch.
(8) Column Actuated Stabilizer Trim Cutout Switch Override Test - Use this test to make sure the
horizontal stabilizer follows the commands from the STAB TRIM switches, even though the
column actuated STAB TRIM cutout switches give the opposite command.
(9) Stabilizer Trim Secondary Brake System Test - Use this test to make sure the stabilizer
secondary brake can prevent movement of the horizontal stabilizer.
(10) Stabilizer Trim Cutout Test - Use this procedure to make sure the stabilizer trim cutout switch
operates correctly. The stabilizer trim cutout switch stops the horizontal stabilizer when the
control column command is opposite from the STAB TRIM switches.
(11) Column Cutout Switches Test - Use this test to make sure the captain’s and first officer’s column
cutout switches operate correctly.
TASK 27-41-00-820-801
2. Stabilizer Control Cable and Chain Adjustment
(Figure 501)
A. General
(1) Use this task to adjust the horizontal stabilizer control cables and chain.
(2) Before you do cable adjustment, permit a minimum of one hour at a constant ambient
temperature of ±5 degrees F (±2.8 degrees C) for the airframe temperature to become stable.
(a) The cable tension values will not be correct when there are temperature differences along
the cable run.
(3) If the cables need to be replaced, do this task: Stabilizer Control Cable Removal,
TASK 27-41-82-000-801.
B. References
Reference Title
27-41-82-000-801 Stabilizer Control Cable Removal (P/B 401)
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EFFECTIVITY
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