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-BBJ)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Reference Description
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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
562 Left Wing - Spoiler No. 5
563 Left Wing - Spoiler No. 4
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
662 Right Wing - Spoiler No. 8
663 Right Wing - Spoiler No. 9
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
D. Prepare for the Test
SUBTASK 27-61-00-860-093
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-00-860-094
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
SUBTASK 27-61-00-480-016
(3) Install the mount, SPL-1670 and the control column assembly protractor, SPL-1680 on the
captain’s aileron control wheel.
SUBTASK 27-61-00-820-022
(4) Adjust the control column assembly protractor, SPL-1680 to zero.
SUBTASK 27-61-00-860-095
(5) Move the speed brake lever to the DOWN position.
SUBTASK 27-61-00-860-096
(6) Put the ailerons in the neutral position.
E. Flight Spoiler System Test
SUBTASK 27-61-00-480-017
(1) Do the steps below in turn for spoiler panels 2, 3, 4 and 5.
(a) Install the protractor, COM-1691 on the spoiler panel.
1) Note the location of the protractor.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-61-00
Page 546
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
2) Adjust the protractor, COM-1691 to zero.
(b) Make sure that rig pin number 15 fits freely in the Aileron Trim Actuator located in the left
main landing gear wheel well.
NOTE: Do not adjust the aileron trim for the remainder of this procedure.
(c) Turn the control wheel counterclockwise to 30 degrees and hold.
1) Using the spoiler protractor, note the position of spoiler panel.
NOTE: If you have to remove the protractor to measure the angle of the spoiler panel,
make sure you replace it in the same location from where it came.
(d) Continue to turn the control wheel counterclockwise to the 87 degree wheel position.
1) Using the spoiler protractor, note the new position of spoiler panel.
(e) Make sure the right wing flight spoiler panels 8, 9, 10 and 11 stay in the full down position.
(f) Shake-out and center the control wheel.
SUBTASK 27-61-00-020-017
(2) Make sure that the noted position of the spoiler panel is within the spoiler position limits as are
shown in the table.
SUBTASK 27-61-00-860-097
(3) Do the following steps:
(a) Turn the control wheel to 87 degrees in the counterclockwise direction.
(b) Slowly turn the control wheel in the clockwise direction.
(c) Stop turning the control wheel when spoiler panels 2, 3, 4 and 5 start to move down.
1) Record the control wheel position.
(d) Slowly begin turning the control wheel to the neutral position.
(e) Stop turning the control wheel when spoiler panels 4 and 5 reach the full down position.
NOTE: In the FULL DOWN position it is normal for spoiler panel 5 to be slightly higher
than spoiler panel 4.
1) Record the control wheel position.
(f) Make sure the noted control wheel positions are within the limits shown in the table below.
Table 504/27-61-00-993-819
Wheel Position 30 +/- 1/2 CCW 87 +/- 1 CCW
Spoiler 2 Position (Degrees) 3.5-4.5 33 +1/-3
Spoiler 3 Position (Degrees) 5.5-6.5 33 +1/-3
Spoiler 4 Position (Degrees) 10.5-11.5 38 +1/-3
Spoiler 5 Position (Degrees) 10.5-11.5 38 +1/-3
Spoilers 8, 9 10, 11 Position Full Down Full Down
SUBTASK 27-61-00-860-099
(4) Shake-out and center the control wheel.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
　
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