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SUBTASK 27-11-51-210-002
(2) Make sure the fork is correctly engaged to the paddle on the control column.
SUBTASK 27-11-51-420-001
(3) Install the control wheel drum assembly [19]:
(a) Connect the cable AA [4] and cable AB [6] to the control wheel drum assembly [19].
(b) Put the end of cable ACBA [1] and cable ACBB [2] through the openings, and at the same
time, put the control wheel drum assembly [19] in its position.
(c) Make sure the radius fillers [8] are bonded to the rib.
(d) Put the bracket [7] in its position with the FWD marking forward.
(e) Install the bracket [7] with the bolts [9], washers [10] and nuts [11].
(f) Install the bolts [12], washers [13], and nuts [14] to attach the control wheel drum
assembly [19] to the airplane structure.
(g) Attach the wiring harness [38] to the control wheel drum assembly [19] with the screws
[31], washers [32], and nuts [34].
(h) Connect the electrical connector [33] to the aileron transmitter.
(i) Connect the electrical connectors [15] and [30] to the roll force transducer [18].
(j) Install the clamps [26], [29] and [41] with screws [24], [27], and [39].
(k) Install the screw [35], and clamp [37] to attach the rudder pedal adjustment crank to the
control wheel drum assembly [19].
SUBTASK 27-11-51-420-002
(4) Install the cable guide [16] to the control wheel drum assembly [19]:
(a) Put the cable guide [16] in its position.
(b) Install the screws [17] on the cable guide [16].
SUBTASK 27-11-51-420-003
(5) Connect the cable AA [4] and cable AB [6] at the turnbuckles [5].
(a) Remove the identification tags from the disconnected cables.
(b) Connect the cable AA [4] and cable AB [6] at the turnbuckles [5].
(c) Tighten the turnbuckles [5] to remove slack but keep the cable tension at zero.
SUBTASK 27-11-51-420-004
(6) Connect the cable ACBA [1] and cable ACBB [2] at the turnbuckles [3]:
(a) Remove the identification tags from the disconnected cables.
(b) Connect the cable ACBA [1] and cable ACBB [2] at the turnbuckles [3].
(c) Tighten the turnbuckles [3] to remove slack but keep the cable tension at zero.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-11-51-080-001
(7) Remove the rig pin A/S-1 and A/S-1A, from the rig pin kit, SPL-1585, from the aileron transfer
mechanism.
SUBTASK 27-11-51-080-002
(8) Remove the rig pin A/S-15, from the rig pin kit, SPL-1585, from the aileron trim mechanism.
SUBTASK 27-11-51-860-003
(9) Do this task: Put the Aileron Hydraulic Systems A and B Back to the Condition Before
Pressure Removal, TASK 27-11-00-860-802.
SUBTASK 27-11-51-820-001
(10) Adjust cables ACBA and ACBB and cables AA and AB. To adjust the cables, do this task:
Aileron Cables Adjustment, TASK 27-11-00-820-801.
SUBTASK 27-11-51-720-001
(11) Do this task: First Officer’s Control Wheel Lost Motion Test, TASK 27-11-00-700-802.
SUBTASK 27-11-51-730-001
(12) Do this task: Manual Reversion Control Friction Test, TASK 27-11-00-700-803.
SUBTASK 27-11-51-710-001
(13) Do this task: Aileron Response (Operational) Test, TASK 27-11-00-710-801.
SUBTASK 27-11-51-720-002
(14) Do this task: Control Wheel Centering Check, TASK 27-11-00-700-804.
SUBTASK 27-11-51-720-003
(15) Do this task: Aileron Control Wheel Force Test, TASK 27-11-00-700-805.
SUBTASK 27-11-51-720-004
(16) Do this task: Control Wheel Travel Stop Test, TASK 27-11-00-700-807.
SUBTASK 27-11-51-710-002
(17) Do this task: Roll Force Transducer Test, TASK 22-11-11-740-801.
SUBTASK 27-11-51-410-001
(18) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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AILERON TRIM ACTUATOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the aileron trim actuator
(2) An installation of the aileron trim actuator.
TASK 27-11-54-000-801
2. Aileron Trim Actuator Removal
(Figure 401)
A. References
Reference Title
27-11-00-860-801 Remove Pressure from the Aileron 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
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(3)
