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Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
C. Prepare for the Check
SUBTASK 27-11-00-860-042
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 553
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-11-00-860-043
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.
D. Do the Centering Check
SUBTASK 27-11-00-720-003
(1) Do the centering check:
(a) Turn the captain’s control wheel clockwise from the neutral position (zero units) to 6 units of
trim.
(b) Turn the captain’s control wheel back to 2 units of trim and release the control wheel.
(c) Make sure the control wheel goes back to the neutral position in 0.0 ±0.4 units of trim
(±2.4 degrees).
(d) Turn the captain’s control wheel counterclockwise from the neutral position (zero units) to 6
units of trim.
(e) Turn the captain’s control wheel back to 2 units of trim and release the control wheel.
(f) Make sure the control wheel goes back to the neutral position in 0.0 ±0.4 units of trim
(±2.4 degrees).
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-11-00-860-044
(1) 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 27-11-00-860-091
(2) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-700-805
12. Aileron Control Wheel Force 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)
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. 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.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 554
Oct 10/2007
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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-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. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Prepare for the Test
SUBTASK 27-11-00-860-045
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-860-046
(2) 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.
SUBTASK 27-11-00-860-047
WARNING: MAKE SURE PERSONS AND EQUIPMENT ARE CLEAR OF ALL FLIGHT CONTROL
SURFACES, THE THRUST REVERSERS AND THE LANDING GEAR. THE FLIGHT
CONTROL SURFACES, THE THRUST REVERSERS AND THE LANDING GEAR CAN
　
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