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E. Column Cutout Switch Removal
SUBTASK 27-41-51-020-001
(1) Remove the nut [6], washer [5], and bolt [4] to disconnect the rod assemblies [8] from the column
cutout switch arms [3].
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SUBTASK 27-41-51-020-002
(2) Do these steps to remove the captain’s column cutout switch [9]:
(a) Disconnect the electrical connectors.
(b) Remove the bolts [1] and washers [2] that attach the captain’s column cutout switch [9] to
the beam assembly.
(c) Remove the captain’s column cutout switch [9].
SUBTASK 27-41-51-020-003
(3) Do these steps to remove the first officer’s column cutout switch [12]:
(a) Disconnect the electrical connectors.
(b) Remove the bolts [10] and washers [11] that attach the first officer’s column cutout switch
[12] to the beam assembly.
(c) Remove the first officer’s column cutout switch [12].
SUBTASK 27-41-51-020-004
(4) If it is necessary, remove the control column position sensor from the column cutout switch. To
remove it, do this task: Control Column Position Sensor Removal, TASK 31-31-52-000-801
------------------------- END OF TASK ---------------------------
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Column Cutout Switch Installation
Figure 401 (Sheet 1 of 3)/27-41-51-990-801
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Column Cutout Switch Installation
Figure 401 (Sheet 2 of 3)/27-41-51-990-801
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Column Cutout Switch Installation
Figure 401 (Sheet 3 of 3)/27-41-51-990-801
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TASK 27-41-51-400-801
3. Column Cutout Switch Installation
(Figure 401)
A. References
Reference Title
27-41-00-700-810 Column Cutout Switches Test (P/B 501)
31-31-52-400-801 Control Column Position Sensor Installation (P/B 401)
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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
G01048 Lockwire - Corrosion Resistant Steel (0.032 In. Dia.) NASM20995~
C32
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
E. Access Panels
Number Name/Location
112A Forward Access Door
F. Column Cutout Switch Installation
SUBTASK 27-41-51-420-001
(1) If it is necessary, install the control column position sensor to the column cutout switch. To install
it, do this task: Control Column Position Sensor Installation, TASK 31-31-52-400-801.
SUBTASK 27-41-51-420-002
(2) Do these steps to install the captain’s column cutout switch [9]:
(a) Put the captain’s column cutout switch [9] in its position.
(b) Install the bolts [1] and washers [2] to attach the captain’s column cutout switch [9] to the
beam assembly.
(c) Connect the electrical connectors.
SUBTASK 27-41-51-420-003
(3) Do these steps to install the first officer’s column cutout switch [12]:
(a) Put the first officer’s column cutout switch [12] in its position.
(b) Install the bolts [10] and washers [11] to attach the first officer’s column cutout switch [12] to
the beam assembly.
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(140)
