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EFFECTIVITY
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Aileron Surface Friction and Motion Test
Figure 507/27-11-00-990-808
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-11-00-700-802
8. First Officer’s Control Wheel Lost Motion Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-11-00-860-801 Remove Pressure from the Aileron Hydraulic Systems A and B
(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)
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)
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
D. Access Panels
Number Name/Location
112A Forward Access Door
E. Prepare for the Test
SUBTASK 27-11-00-860-032
(1) Do this task: Remove Pressure from the Aileron Hydraulic Systems A and B,
TASK 27-11-00-860-801.
SUBTASK 27-11-00-860-033
(2) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-010-003
(3) Open this access panel:
Number Name/Location
112A Forward Access Door
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-860-034
(4) Make sure you can freely install and remove the rig pin A/S-15, from the rig pin kit, SPL-1585, in
the aileron trim actuator (Figure 501).
SUBTASK 27-11-00-480-013
(5) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 to the first
officer’s control wheel.
(a) Set the indicator on the control column assembly protractor, SPL-1680 to zero degrees.
F. First Officer’s Control Wheel Lost Motion Test
SUBTASK 27-11-00-720-002
(1) Do a lost motion test of the first officer’s control wheel:
(a) Make sure you can freely install the rig pin A/S-3, from the rig pin kit, SPL-1585, in the
aileron input crank (Figure 501).
(b) Turn the first officer’s control wheel clockwise from the neutral position to the lost motion
device stop.
1) Make sure the control wheel turns 12 ±1 degrees from the neutral position.
(c) Turn the first officer’s control wheel counterclockwise from the neutral position to the lost
motion device stop.
1) Make sure the control wheel turns 12 ±1 degrees from the neutral position.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-11-00-080-009
(1) Remove the mount, SPL-1670 and the control column assembly protractor, SPL-1680 from the
first officer’s control wheel.
SUBTASK 27-11-00-080-010
(2) Remove the rig pin A/S-3, from the rig pin kit, SPL-1585, from the pogo lever.
SUBTASK 27-11-00-860-035
(3) Do this task: Put the Aileron Hydraulic Systems A and B Back to the Condition Before
Pressure Removal, TASK 27-11-00-860-802.
SUBTASK 27-11-00-010-004
(4) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
TASK 27-11-00-700-803
9. Manual Reversion Control Friction 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)
　
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