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down direction. The force is to be applied to the top side of the tab leading edge.
1) Make a record of the travel shown on the dial indicator.
(k) Slowly remove the force.
(l) Make sure that the sum of the two travel records is not more than 0.030 inch (0.76
millimeter).
1) If the sum of the two travel records is more than 0.030 inch (0.72 millimeter) check the
hinges for excessive wear and replace, as necessary.
(m) Move the mounting plate and dial indicator to the next hinge centerline.
(n) Repeat the above steps for each of the other three outboard elevator tab hinges.
(o) Repeat the above steps for the 4 hinges on the tab of the opposite elevator.
(p) Remove the dial indicator.
(q) Remove the mounting plate.
SUBTASK 27-31-32-640-001
(2) Lubricate the elevator tab hinges, do this task: Elevator Tab Hinge Lubrication,
TASK 12-22-31-640-802.
J. Put the Airplane Back to Its Usual Condition.
SUBTASK 27-31-32-860-006
(1) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-32-410-001
(2) Install this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
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Elevator Tab Freeplay Check
Figure 602 (Sheet 1 of 6)/27-31-32-990-802
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EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
Page 611
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Elevator Tab Freeplay Check
Figure 602 (Sheet 2 of 6)/27-31-32-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
Page 612
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Elevator Tab Freeplay Check
Figure 602 (Sheet 3 of 6)/27-31-32-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
Page 613
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Elevator Tab Freeplay Check
Figure 602 (Sheet 4 of 6)/27-31-32-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
Page 614
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Elevator Tab Freeplay Check
Figure 602 (Sheet 5 of 6)/27-31-32-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
Page 615
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Elevator Tab Freeplay Check
Figure 602 (Sheet 6 of 6)/27-31-32-990-802
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-32
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GUN 156, 201-204, 206 PRE SB 737-55A1080 (Continued)
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
TASK 27-31-32-200-802
4. Elevator Tab Freeplay - Check
(Figure 603)
A. General
(1) Use this test to do a check of the elevator tab trailing edge freeplay, the elevator tab hinge line
axial freeplay, and the elevator tab hinge line radial freeplay.
B. References
Reference Title
12-22-31-640-802 Elevator Tab Hinge Lubrication (P/B 301)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-801 Put the Elevator Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (P/B 201)
C. 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.
　
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