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737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 549
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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-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)
STD-1293 Wrench - Torque (100 Lb-In)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
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
572 Left Wing - Aileron
672 Right Wing - Aileron
D. Prepare for the Test
SUBTASK 27-11-00-860-036
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-480-014
(2) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 to the first
officer’s control wheel.
SUBTASK 27-11-00-480-015
(3) Install the adapter, SPL-1674 to the captain’s control wheel.
SUBTASK 27-11-00-860-037
(4) Make sure the aileron trim system is at the center.
SUBTASK 27-11-00-860-038
(5) Set the control column assembly protractor, SPL-1680 to zero degrees.
E. Manual Reversion Control Friction Test
SUBTASK 27-11-00-730-001
(1) Do the manual reversion control friction test:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 550
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(a) Use the torque wrench (100 Lb-In), STD-1293 on the adapter, SPL-1674 to measure the force
that is necessary to turn the captain’s control wheels in the clockwise direction.
NOTE: If the adapter, SPL-1674 is not available, apply a tangent force to the captain’s
control wheel at 6.5 inch (165 millimeters) radius.
1) Turn the control wheel clockwise until the ailerons start to move.
a) Make sure the force is not more than 215 pound-inches (24.3 newton-meters) or
33.1 pounds (147.2 newtons).
2) Continue to turn the control wheel to 20 degrees.
a) Make sure the force is not more than 243 pound-inches (27.5 newton-meters) or
37.4 pounds (166.4 newtons).
3) Continue to turn the control wheel to 40 degrees.
a) Make sure the force is not more than 279 pound-inches (31.5 newton-meters) or
42.9 pounds (190.8 newtons).
4) Continue to turn the control wheel to 75 degrees.
a) Make sure the force is not more than 333 pound-inches (37.6 newton-meters) or
51.2 pounds (227.7 newtons).
(b) Measure the force that is necessary to turn the captain’s control wheel in the
counterclockwise direction.
NOTE: If the adapter, SPL-1674 is not available, apply a tangent force to the captain’s
control wheel at 6.5 inch (165 millimeters) radius.
1) Turn the control wheel counterclockwise until the ailerons start to move.
a) Make sure the force is not more than 215 pound-inches (24.3 newton-meters) or
33.1 pounds (147.2 newtons).
2) Continue to turn the control wheel to 20 degrees.
a) Make sure the force is not more than 243 pound-inches (27.5 newton-meters) or
37.4 pounds (166.4 newtons).
3) Continue to turn the control wheel to 40 degrees.
a) Make sure the force is not more than 279 pound-inches (31.5 newton-meters) or
42.9 pounds (190.8 newtons).
4) Continue to turn the control wheel to 75 degrees.
a) Make sure the force is not more than 333 pound-inches (37.6 newton-meters) or
51.2 pounds (227.7 newtons).
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册1(118)
