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(c) Make sure the total side play of the control column assembly is 0.01-0.03 inch (0.25-0.76
millimeter).
(d) Make sure the outboard end of the stop on the left side of the forward quadrant assembly
[1] is clear of the inboard face of the bracket by 0.07-0.24 inch (1.8-6.1 millimeters).
(e) If necessary, add or remove shim under the bearing housing.
SUBTASK 27-31-61-420-003
(6) Install the ring assemblies and dust seals:
(a) Install the forward dust seals [26], aft dust seals [25], forward ring assemblies [21], and aft
ring assemblies [24] with the screws [22] and washers [23].
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CAUTION: DO NOT HOLD THE DUST CAP TOO TIGHTLY AGAINST THE WIRE BUNDLE. IT
CAN CAUSE DAMAGE TO THE ELECTRICAL WIRES.
(b) If it is necessary, adjust the dust cap [20] to set the edge of the dust seals lightly up against
the dust caps [20].
1) Loosen the clamps to adjust the dust caps [20].
(c) Make sure the gap between the two dust seals is 0.60 inch (15.2 millimeters).
(d) Fill the gap between the two dust seals with compound, A00225.
(e) Fill the hole between the notch in the dust seals and the cutout in the floor with compound,
A00225.
SUBTASK 27-31-61-080-002
(7) Remove the rig pin E-1 from the rig pin kit, SPL-1585 from the left side of the forward quadrant
assembly.
SUBTASK 27-31-61-710-001
(8) Do a check of the control column:
(a) Move the control column full forward then full aft.
1) Make sure the control column operates correctly and smoothly.
SUBTASK 27-31-61-420-004
(9) Connect the cables EA [2] and cables EB [3] to the forward quadrants assembly [1]
(a) Install the bolts [6], washers [7], and nuts [8] that attach the fairleads [9] to forward
quadrant assembly [1].
(b) Remove the identification tags from the cable EA [2] and cable EA [3].
(c) Install the cables EA [2] and cables EB [3] to the forward quadrants assembly [1].
(d) Install the retainers [4] and screws [10] to the cables EA [2] and cables EB [3].
(e) Remove the control cable clamp, SPL-1569 if installed.
SUBTASK 27-31-61-080-003
(10) Remove the rig pin E-5 from the rig pin kit, SPL-1585 from the aft control quadrant (Figure 401).
SUBTASK 27-31-61-420-005
(11) Install the pitch control wheel steering force transducers to the forward quadrant assembly. To
install them, do this task: Pitch Force Transducer Installation, TASK 22-11-92-400-801.
SUBTASK 27-31-61-860-002
(12) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
SUBTASK 27-31-61-820-002
(13) Adjust the elevator control cables EA and EB. To adjust them, do this task: Elevator Control
Cables EA and EB and Pitch Force Transducers - Adjustment, TASK 27-31-00-820-801.
SUBTASK 27-31-61-710-002
(14) Do this task: Manual Mode - Test, TASK 27-31-00-700-807.
G. Put the Airplane Back To Its Usual Condition
SUBTASK 27-31-61-410-001
(1) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
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SUBTASK 27-31-61-410-002
(2) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
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ELEVATOR FORWARD CONTROL QUADRANT ASSEMBLY - INSPECTION/CHECK
1. General
A. This procedure has this inspection task:
(1) Elevator Mechanical Control Path
TASK 27-31-61-210-801
2. Elevator Mechanical Control Path Inspection
A. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
317 Tail Cone Compartment - Left
318 Tail Cone Compartment - Right
B. Access Panels
Number Name/Location
112A Forward Access Door
318BR Tailcone Access Door
C. Procedure
SUBTASK 27-31-61-010-003
(1) To get access to the elevator mechanical control path, do this task:
Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-31-61-210-001
(2) Do a general visual inspection of the forward elevator mechanical control path.
SUBTASK 27-31-61-410-003
　
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