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-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
D. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
F. Prepare for the Adjustment
SUBTASK 27-31-00-860-040
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-860-041
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
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SUBTASK 27-31-00-860-042
(3) Open this circuit breaker and install safety tag:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 2 C00849 AFCS STABILIZER TRIM
SUBTASK 27-31-00-010-006
(4) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-043
(5) Use the bar, SPL-1677 to set the "B" dimension at 4 units of trim (39.89 +/- 0.01 inches or 1013.2
+/- 0.3 mm) (Figure 502).
G. Input Rod of the Elevator Feel Computer Adjustment
SUBTASK 27-31-00-410-006
(1) Make sure you can install the rig pin E-4 from the rig pin kit, SPL-1585 in the rig pin holes in the
input arm [122] and elevator feel computer [127].
SUBTASK 27-31-00-820-010
(2) If you can not install the rig pin E-4 easily, adjust the input rod [121] of the elevator feel computer
[127] (Figure 513):
(a) Remove the nut [125], washer [124], and bolt [123] to disconnect the input rod [121] from the
input arm [122].
(b) Install the rig pin E-4 in the rig pin holes in the input arm [122] and elevator feel computer
[127].
(c) Loosen the checknut [126].
(d) Adjust the input rod [121] until you can install the bolt [123] easily through the input arm
[122] and input rod [121].
(e) Install the washer [124] and nut [125].
(f) Tighten the checknut [126].
(g) Remove the rig pin E-4.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-044
(1) Remove the safety tag and close this circuit breaker:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 2 C00849 AFCS STABILIZER TRIM
SUBTASK 27-31-00-820-011
(2) Do this task: Stabilizer Position Sensor Test, TASK 22-11-31-710-801.
SUBTASK 27-31-00-410-007
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
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SUBTASK 27-31-00-860-045
(4) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
------------------------- END OF TASK ---------------------------
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Elevator Feel Computer Input Rod Adjustment
Figure 513 (Sheet 1 of 2)/27-31-00-990-812
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Elevator Feel Computer Input Rod Adjustment
Figure 513 (Sheet 2 of 2)/27-31-00-990-812
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TASK 27-31-00-700-802
12. Elevator Surface Friction and Balance - Test
(Figure 502) (Figure 505)
A. General
(1) Use this test to make sure the elevators are balanced.
B. References
Reference Title
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
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)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
　
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