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SUBTASK 27-61-00-710-002
(1) Turn the captain’s aileron control wheel fully counterclockwise.
(a) Make sure the override mechanism (within the spoiler mixer) is operating properly.
NOTE: This operational test checks the internal function of the spoiler mixer unit. The left
spoiler output quadrant, lever and spoiler ratio changer input rod must all move
together with no override breakout or mechanical interference.
SUBTASK 27-61-00-710-005
(2) Turn the captain’s aileron control wheel fully clockwise.
(a) Make sure the override mechanism (within the spoiler mixer) is operating properly.
NOTE: This operational test checks the internal function of the spoiler mixer unit. The
right spoiler output quadrant, lever and spoiler ratio changer input rod must all
move together with no override breakout or mechanical interference.
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SUBTASK 27-61-00-710-003
(3) Turn the captain’s aileron control wheel fully counterclockwise and hold.
(a) Make sure the No. 2, 3, 4, and 5 flight spoilers move to the up position.
SUBTASK 27-61-00-710-006
(4) Release the captain’s control wheel.
(a) Make sure the No. 2, 3, 4, and 5 flight spoilers move to the down position.
SUBTASK 27-61-00-710-004
(5) Turn the captain’s aileron control wheel fully clockwise and hold.
(a) Make sure the No. 8, 9, 10 and 11 flight spoilers move to the up position.
SUBTASK 27-61-00-710-007
(6) Release the captain’s control wheel.
(a) Make sure the No. 8, 9, 10, and 11 flight spoilers move to the down position.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-61-00-860-078
(1) Do this task: Put the Spoiler Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-61-00-840-801.
------------------------- END OF TASK ---------------------------
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SPOILER CONTROL SYSTEM - INSPECTION/CHECK
TASK 27-61-00-210-801
1. Spoiler Wheel Well Mechanical Components Inspection
(Figure 601)
A. General
(1) This task is a general visual inspection of the spoiler mechanical components in the wheel well.
B. References
Reference Title
25-22-00-000-801 Passenger Seat Removal (P/B 401)
25-22-00-400-802 Passenger Seat Installation (P/B 401)
25-27-15-000-801 Carpet Removal (P/B 401)
25-27-15-400-801 Carpet Installation (P/B 401)
53-21-00-000-801 Passenger Cabin Floor Panel Removal (P/B 401)
53-21-00-400-801 Passenger Cabin Floor Panel Installation (P/B 401)
C. Location Zones
Zone Area
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
232 Forward Passenger Compartment - Forward Entry Door to Sta 663.75
- Right
D. Procedure
SUBTASK 27-61-00-210-004
(1) Inspect the spoiler mechanical components in the wheel well (Figure 601).
(a) Do a general visual inspection of all spoiler mechnical components, including the
following:
1) Spoiler mixer
2) Spoiler ratio changer and input rod
3) Spoiler control quadrant shaft
4) Aileron spring cartridge
SUBTASK 27-61-00-210-005
(2) Inspect the spoiler control quadrant.
(a) Remove the right floor panel between the seat tracks at the second window aft of the wing
escape hatch:
1) Do this task: Passenger Seat Removal, TASK 25-22-00-000-801.
2) Do this task: Carpet Removal, TASK 25-27-15-000-801.
3) Do this task: Passenger Cabin Floor Panel Removal, TASK 53-21-00-000-801.
(b) Do a general visual inspection of the spoiler control quadrant.
(c) Install the right floor panel:
1) Do this task: Passenger Cabin Floor Panel Installation, TASK 53-21-00-400-801.
2) Do this task: Carpet Installation, TASK 25-27-15-400-801.
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3) Do this task: Passenger Seat Installation, TASK 25-22-00-400-802.
------------------------- END OF TASK ---------------------------
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(26)
