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318BR Tailcone Access Door
SUBTASK 27-31-81-480-001
(3) Use the bar, SPL-1677 to set the B dimension at 39.89 +/- 0.01 inches (1013.2 +/- 0.3
millimeters) (Figure 402).
SUBTASK 27-31-81-860-001
(4) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-81-860-002
(5) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-81-480-002
(6) Attach DO-NOT-OPERATE tags to the control columns.
SUBTASK 27-31-81-480-003
(7) Use the beam, SPL-1730 to adjust the elevator trailing edge (Figure 403):
(a) Set the beam, SPL-1730 on the stabilizer lower surface.
(b) Set the elevator trailing edge to the index mark on the beam, SPL-1730.
(c) Remove the beam, SPL-1730.
H. Elevator Index Plate Installation
(Figure 401)
SUBTASK 27-31-81-420-001
(1) Install the elevator index plate [1]:
(a) Align the center mark of elevator index plate [1] with the elevator trailing edge.
(b) Drill two 0.190 +0.004/-0.000 inch (4.82 +0.10/-0.00 millimeters) diameter holes through the
tail cone and the elevator index plate [1].
(c) Install the bolts [2], washers [3], and nuts [4] to attach the elevator index plate [1] to the tail
cone.
(d) Install the lockwire, G01912.
SUBTASK 27-31-81-080-001
(2) Remove the DO-NOT-OPERATE tags from the control columns.
SUBTASK 27-31-81-210-001
(3) Make sure the elevator trailing edge aligns with the center mark of the elevator index plate.
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I. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-81-410-001
(1) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-81-410-002
(2) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-81-860-003
(3) 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 Index Plate Installation
Figure 402/27-31-81-990-802
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Rigging Beam Installation
Figure 403 (Sheet 1 of 2)/27-31-81-990-803
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Rigging Beam Installation
Figure 403 (Sheet 2 of 2)/27-31-81-990-803
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ELEVATOR NEUTRAL SHIFT MECHANISM - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the elevator neutral shift mechanism
(2) An installation of the elevator neutral shift mechanism.
B. The elevator neutral shift mechanism is referred to as the "neutral shift mechanism" in this
procedure.
TASK 27-31-91-000-801
2. Elevator Neutral Shift Mechanism Removal
(Figure 401, Figure 402)
A. References
Reference Title
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
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-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
SPL-1672 Assembly - Lock, Stabilizer Trim
(Part #: F71336-501, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
　
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