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A. References
Reference Title
22-11-41-400-801 Autopilot Disengage Switch Installation (P/B 401)
23-51-04-400-801 Control Wheel PTT Switch Installation (P/B 401)
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-11-00-860-802 Put the Aileron Hydraulic Systems A and B Back to the Condition
Before Pressure Removal (P/B 201)
27-41-97-400-801 Stabilizer Trim Control Switch 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-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-1671 Straightedge - Control Wheel
(Part #: SE27-0001, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1674 Assembly - Adapter, Control Wheel, Torque and Force Test
(Part #: F72867-1, 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. Consumable Materials
Reference Description Specification
A00900 Sealant - Silicone, RTV - Dow Corning 93-006-1
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
3 Control wheel 27-31-51-03-055 GUN 001-030, 101-122,
155-157, 201-999
27-31-51-03-201 GUN 001-026, 101-120,
155-157, 201-999
E. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-41
Page 407
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
F. Access Panels
Number Name/Location
112A Forward Access Door
G. Aileron Control Wheel Installation
SUBTASK 27-11-41-020-005
(1) If you removed the stabilizer trim control switch, do this task: Stabilizer Trim Control Switch
Installation, TASK 27-41-97-400-801.
SUBTASK 27-11-41-020-006
(2) If you removed the autopilot disengage switch, do this task: Autopilot Disengage Switch
Installation, TASK 22-11-41-400-801.
SUBTASK 27-11-41-020-007
(3) If you removed the control wheel PTT switch, do this task: Control Wheel PTT Switch
Installation, TASK 23-51-04-400-801.
SUBTASK 27-11-41-420-001
(4) Install the aileron control wheel [3] (Figure 402):
(a) Install the terminal block [17] in the hub of the wheel.
(b) Install the screws [19], washers [18] and washers [20] to connect the terminals of the switch
wires to the terminal block [17].
(c) Make sure the terminals of the switch wires are installed correctly.
(d) Attach the terminal cover [16] to the aileron control wheel [3] with washers [13] and
screws [12].
(e) Apply Dow Corning 93-006-1 sealant, A00900 to the wire bundle and the control wheel
splines.
(f) Use a wire leader to put the electrical wires in the aileron control wheel [3].
(g) Put a clamp [15] at the mark on the wire bundle.
CAUTION: MAKE SURE THE WIRE BUNDLE LENGTH IS CORRECT BETWEEN THE AILERON
CONTROL COLUMN AND THE AILERON CONTROL WHEEL. THE AILERON
CONTROL WHEEL CAN NOT MOVE FREELY IF THE WIRE BUNDLE IS NOT
CORRECT. THIS CAN CAUSE DAMAGE TO THE WIRE BUNDLE INSIDE THE
AILERON CONTROL WHEEL.
(h) Make sure the length of the wire bundle is approximately 27 inches (685.8 millimeters)
between the clamp [15] in the aileron control wheel [3] and the hole in the housing.
(i) Make sure the aileron control wheel [3] moves an equal distance each direction from the
neutral position.
(j) Install the clamp [15] with the screw [14] to hold the wire bundle to the aileron control
wheel [3].
(k) Wind the wire bundle four times around the control wheel hub.
NOTE: As you look forward into the control wheel upper cavity, wind the wire bundle
counterclockwise for the captain’s aileron control wheel. For the first officer’s
aileron control wheel, wind the wire bundle clockwise. Fig. 402, Detail (B).
　
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