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(j) Turn and hold the captain’s control wheel at 75 degrees counterclockwise.
1) Make sure the control wheel moves freely through travel.
2) Make sure the force to hold the control wheel is not more than 137 pound-inches (15.5
newton-meters) or 21 pounds (93.4 newtons) at 6.5 inches (165 millimeters) radius.
(k) Release the captain’s control wheel.
1) Make sure the control wheel goes back to the trim position of 57 degrees minimum
clockwise.
(l) At the same time, operate the aileron trim switches in the LEFT WING DOWN direction until
the trim actuator stops.
1) Make sure the control wheel turns counterclockwise a minimum of 9.5 trim indicator
units.
(m) Manually turn the captain’s control wheel 105 degrees counterclockwise.
(n) Turn the captain’s control wheel back to the neutral position.
(o) Turn and hold the captain’s control wheel at 75 degrees clockwise.
1) Make sure the control wheel moves freely through travel.
2) Make sure the force to hold the control wheel is not more than 137 pound-inches (15.5
newton-meters) or 21 pounds (93.4 newtons) at 6.5 inches (165 millimeters) radius.
(p) Release the captain’s control wheel.
1) Make sure the control wheel goes back to the trim position of 57 degrees minimum
counterclockwise.
(q) At the same time, operate the aileron trim switches to put the control wheels at
approximately 0 units of trim.
(r) Operate one aileron trim switch in the LEFT WING DOWN direction then the RIGHT WING
DOWN direction.
1) Make sure the control wheels do not move.
(s) Operate the other aileron trim switch in the LEFT WING DOWN direction then the RIGHT
WING DOWN direction.
1) Make sure the control wheels do not move.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-11-00-080-018
(1) Remove the adapter, SPL-1674 from the captain’s aileron control wheel.
SUBTASK 27-11-00-080-019
(2) Remove the mount, SPL-1670 and the control column assembly protractor, SPL-1680 from the
first officer’s control wheel.
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SUBTASK 27-11-00-860-051
(3) To remove power from hydraulic systems A and B, do this task: Hydraulic System A or B
Power Removal, TASK 29-11-00-860-805.
SUBTASK 27-11-00-860-093
(4) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-710-802
14. Aileron Spring Cartridge and Transfer Mechanism Operational Test
(Figure 501)
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)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Prepare for the Test
SUBTASK 27-11-00-860-064
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-860-065
WARNING: MAKE SURE ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THE CONTROL
SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR CAN MOVE
SUDDENLY WITH THE PRESSURIZATION OF A HYDRAULIC SYSTEM. THIS CAN
CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Pressurize hydraulic systems A and B, do this task: Hydraulic System A or B Pressurization,
TASK 29-11-00-860-801.
SUBTASK 27-11-00-210-005
(3) Make sure the FLT CONTROL A and B switches, on the forward overhead panel P5, are ON.
SUBTASK 27-11-00-860-066
(4) Make sure that the aileron trim control system is at the neutral position.
D. Aileron Spring Cartridge and Transfer Mechanism Operational Test
SUBTASK 27-11-00-710-003
(1) Do the operational test of the spring cartridge and the transfer mechanism:
(a) Operate the two aileron trim switches to put the aileron control wheels to the neutral (zero
unit) position.
(b) Shake the control wheel to center the aileron system.
(c) Turn the captain’s control wheel fully clockwise and hold.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 560
Oct 10/2007
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(d) Turn the first officer’s control wheel counterclockwise through neutral and beyond 10 units
left aileron, and return the control wheel to neutral.
　
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