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(1) Put the captain’s and first officer’s control wheels in the neutral position.
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SUBTASK 27-61-41-860-002
(2) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-61-41-860-003
(3) Install the rig pins A/S-1 and A/S-1A from the test set rig pin kit, SPL-1585 in the aileron transfer
mechanism.
(a) Make sure the rig pin A/S-1 is fully installed in the aileron transfer mechanism and will not
fall out.
SUBTASK 27-61-41-860-004
(4) Remove the right floor panel between the seat tracks at the second window aft of the wing
escape hatch:
(a) Do this task: Passenger Seat Removal, TASK 25-22-00-000-801.
(b) Do this task: Carpet Removal, TASK 25-27-15-000-801.
(c) Do this task: Passenger Cabin Floor Panel Removal, TASK 53-21-00-000-801.
F. Spoiler Control Quadrant Removal
SUBTASK 27-61-41-020-001
(1) Disconnect aileron control cable AA [1] and cable AB [3]:
(a) Install the turnbuckle clamps on the cable AA [1] and cable AB [3] to keep a small tension
when you disconnect the cable turnbuckles [2].
(b) Disconnect the cable turnbuckles [2].
(c) Remove cable AA [1] and cable AB [3] from the spoiler cable quadrant [5].
(d) Install a tag on cable AA [1] and cable AB [3] for identification during the installation.
SUBTASK 27-61-41-020-002
(2) Remove the spoiler cable quadrant [5].
(a) Remove nuts [9], washers [8], washers [7] and bolts [6] that attach the spoiler cable
quadrant [5] to the quadrant shaft [36].
(b) Remove the nut [19], washer [18], washer [17] and bolt [16] that attaches the ratio changer
input rod [35] to the upper control crank [15].
(c) Remove the nut [30], washer [29], washer [28] and bolt [27] that attaches the aileron spring
cartridge [31] to the aileron input crank [26].
(d) Remove the nuts [24], washers [23], washers [22] and bolts [21] that attach the quadrant
shaft support bracket [25] to the forward bulkhead [20].
(e) Remove the nuts [14], washers [13], washers [12] and bolts [11] that attach the bearing
retainer [38] to the wheel well ceiling [37].
(f) Break the pressure seal between the bearing retainer [38] and the wheel well ceiling [37].
(g) Disconnect the quadrant shaft [36] from the spoiler control quadrant [5].
(h) Lower the quadrant shaft [36] from the wheel well ceiling [37] and remove it from the
airplane.
(i) Remove the spoiler cable quadrant [5] from the airplane.
------------------------- END OF TASK ---------------------------
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Spoiler Control Quadrant Installation
Figure 401 (Sheet 1 of 5)/27-61-41-990-801
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Spoiler Control Quadrant Installation
Figure 401 (Sheet 2 of 5)/27-61-41-990-801
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Spoiler Control Quadrant Installation
Figure 401 (Sheet 3 of 5)/27-61-41-990-801
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Spoiler Control Quadrant Installation
Figure 401 (Sheet 4 of 5)/27-61-41-990-801
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Spoiler Control Quadrant Installation
Figure 401 (Sheet 5 of 5)/27-61-41-990-801
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TASK 27-61-41-400-801
3. Spoiler Control Quadrant Installation
(Figure 401)
A. References
Reference Title
25-22-00-400-802 Passenger Seat Installation (P/B 401)
25-27-15-400-801 Carpet Installation (P/B 401)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(44)
