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Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
24-22-00-860-812 Remove Electrical Power (P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1670 Mount - Control Wheel Protractor
(Part #: F72790, Supplier: 81205, A/P Effectivity: 737-100, -200, -200C,
-300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900, -900ER,
-BBJ)
SPL-1680 Protractor - Assembly, Control Column
(Part #: 4MIT65B80307-1, Supplier: 81205, A/P Effectivity: 737-100,
-200, -200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800,
-900, -900ER, -BBJ)
(Part #: A27021-29, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 564
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
D. Do a Test of the Control Wheel Travel Stop
SUBTASK 27-11-00-480-025
(1) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 on the first
officer’s control wheel.
(a) Set the indicator on the control column assembly protractor, SPL-1680 to zero degree.
SUBTASK 27-11-00-860-056
(2) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-720-005
(3) Do the test of the control wheel travel stop:
(a) Turn the captain’s control wheel clockwise until the control column stops touch.
1) Make sure the first officer’s control wheel turns a minimum of 105 degrees.
NOTE: A minimum of 105 degrees control wheel travel is required for the captain’s
control wheel to touch the forward stop. This large deflection can be
necessary for certain flight conditions in manual reversion.
The system reaches the aft quadrant stop at approximately 90 degrees.
Additional force will be necessary to stretch the control cable past 90 degrees
until the control column stops touch.
(b) Turn the captain’s control wheel counterclockwise until the control column stops touch.
1) Make sure the first officer’s control wheel moves freely and turns a minimum of 105
degrees.
NOTE: Turn the control wheel 105 degrees clockwise to make sure the minimum
travel requirements of the control wheel are met and that there are no
obstructions in the control column and control wheel installations. A minimum
of 105 degrees control wheel travel is required for the captain’s control wheel
to touch the forward stop. This large deflection can be necessary for certain
flight conditions in manual reversion. The system reaches the aft stops at
approximately 90 degrees. Apply additional force to turn the control wheel
more than 90-95 degrees. The control cables stretch slightly when the control
wheels are turned beyond 90 degrees.
SUBTASK 27-11-00-860-096
(4) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
SUBTASK 27-11-00-080-021
(5) Remove the control column assembly protractor, SPL-1680 and the mount, SPL-1670 from the
first officer’s control wheel.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-700-810
17. Control Wheel Travel Interference Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
24-22-00-860-812 Remove Electrical Power (P/B 201)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 565
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Control Wheel Travel Interference Test
SUBTASK 27-11-00-860-100
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-700-002
(2) Do the test of the control wheel travel interference:
(a) Hold the control column full forward and do the following steps:
1) Turn the control wheel to the full left (counterclockwise) position.
2) Make sure the control wheel travel is smooth through the full turn.
3) Turn the control wheel to the center position.
4) Turn the control wheel to the full right (clockwise) position.
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(126)
