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5) Make sure the control wheel travel is smooth through the full turn.
6) Turn the control wheel to the center position.
(b) Hold the control column full aft and do the following steps:
1) Turn the control wheel to the full left (counterclockwise) position.
2) Make sure the control wheel travel is smooth through the full turn.
3) Turn the control wheel to the center position.
4) Turn the control wheel to the full right (clockwise) position.
5) Make sure the control wheel travel is smooth through the full turn.
6) Turn the control wheel to the center position.
7) Return the control column to the neutral position.
SUBTASK 27-11-00-860-101
(3) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
------------------------- END OF TASK ---------------------------
TASK 27-11-00-700-808
18. Aileron Balance Tab Position 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)
B. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
572 Left Wing - Aileron
672 Right Wing - Aileron
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 566
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
C. Aileron Balance Tab Position Test
SUBTASK 27-11-00-860-057
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-11-00-720-006
(2) Do a test of the position of the aileron LEFT balance tab:
NOTE: For all aileron tab measurements in this test, measure the distances from the LOWER
surface of the aileron tab at the tip of the trailing edge to the LOWER surface of the
aileron at the tip of the trailing edge.
(a) Set the aileron at the rig position (Figure 506).
NOTE: The aileron rig position is when the outboard edge of the aileron upper surface is
0.49 ±0.03 inch (12.4 ±0.8 millimeters) below the adjacent fixed lower trailing
edge surface.
(b) Measure the vertical distance from the tip of the outboard trailing edge of the aileron tab to
the tip of the adjacent aileron trailing edge.
GUN 101-122
1) Make sure the distance is 0.12 ±0.07 inch (3.05 ±1.8 millimeter).
GUN 001-099, 155-157, 201-999
2) Make sure the distance is 0.06 ±0.07 inch (1.5 ±1.8 millimeter).
GUN 101-122
(c) Manually move the aileron DOWN so that the tip of the outboard lower trailing edge of the
aileron is 3.63 ±0.01 inches (92.2 ±0.25 millimeters) below the tip of the lower trailing
edge of the adjacent fixed trailing edge surface.
GUN 001-099, 155-157, 201-999
(d) Manually move the aileron DOWN so that the tip of the outboard lower trailing edge of the
aileron is 3.39 ±0.01 inches (86.1 ±0.25 millimeters) below the tip of the lower trailing
edge of the adjacent fixed trailing edge surface.
GUN ALL
(e) Measure the distance from the tip of the lower surface of the aileron tab to the tip of the
lower surface of the adjacent aileron trailing edge.
GUN 101-122
1) Make sure the aileron balance tab moves UP 0.92 ±0.01 inch (23.4 ±0.25 millimeters) .
GUN 001-099, 155-157, 201-999
2) Make sure the aileron balance tab moves UP 0.86 ±0.01 inch (21.8 ±0.25 millimeters) .
GUN 101-122
(f) Manually move the aileron UP so that the tip of the outboard lower trailing edge of the
aileron is 4.35 ±0.01 inches (110.5 ±0.25 millimeters) above the tip of the lower trailing
edge of the adjacent fixed trailing edge surface.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-11-00
Page 567
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 101-122 (Continued)
GUN 001-099, 155-157, 201-999
(g) Manually move the aileron UP so that the tip of the outboard lower trailing edge of the
aileron is 4.59 ±0.01 inches (116.6 ±0.25 millimeters) above the tip of the lower trailing
edge of the adjacent fixed trailing edge surface.
GUN ALL
(h) Measure the distance from the tip of the lower surface of the aileron tab to the tip of the
lower surface of the adjacent aileron trailing edge.
GUN 101-122
1) Make sure the aileron balance tab moves DOWN 1.10 ±0.01 inch (27.9 ±0.25
millimeters) .
GUN 001-099, 155-157, 201-999
2) Make sure the aileron balance tab moves DOWN 1.16 ±0.01 inch (29.5 ±0.25
millimeters) .
GUN ALL
SUBTASK 27-11-00-720-007
　
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