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(3) Release the PCU input lever [3].
(a) Verify that the hub assembly [1] rotates back to the neutral position.
(b) Verify that the follower arm [2] returns to center.
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SUBTASK 27-61-00-700-020
(4) Repeat the procedure, as necessary, for spoilers 2, 3, 4, 5, 8, 9, 10, and 11.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-61-00-860-083
(1) Remove rig pin A/S-15 from the aileron feel and centering unit.
(2) Remove the plastic tie strap from the input lever [3].
SUBTASK 27-61-00-860-091
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU INSTALL HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU INSTALL HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-61-00-860-084
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU EXTEND THE FLAPS. CONTROL SURFACES CAN MOVE
QUICKLY WHEN YOU MOVE THE FLAPS LEVER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(4) Return the flaps to the retracted position. To retract them, do this task: Extend the Trailing Edge
Flaps, TASK 27-51-00-860-803.
SUBTASK 27-61-00-860-092
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU REMOVE HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU REMOVE HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(5) Do this task: Remove Pressure from the Speed Brake Hydraulic Systems A and B,
TASK 27-62-00-800-802.
------------------------- END OF TASK ---------------------------
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Flight Spoiler Actuator Override Quadrant Operational Test
Figure 506 (Sheet 1 of 3)/27-61-00-990-810
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Flight Spoiler Actuator Override Quadrant Operational Test
Figure 506 (Sheet 2 of 3)/27-61-00-990-810
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Flight Spoiler Actuator Override Quadrant Operational Test
Figure 506 (Sheet 3 of 3)/27-61-00-990-810
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TASK 27-61-00-710-802
16. Spoiler Mixer Centering Mechanism Operational Test
A. References
Reference Title
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
B. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
562 Left Wing - Spoiler No. 5
563 Left Wing - Spoiler No. 4
564 Left Wing - Spoiler No. 3
565 Left Wing - Spoiler No. 2
662 Right Wing - Spoiler No. 8
663 Right Wing - Spoiler No. 9
664 Right Wing - Spoiler No. 10
665 Right Wing - Spoiler No. 11
C. Prepare for the Test
SUBTASK 27-61-00-860-077
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do this task:Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801 .
D. Spoiler Mixer Centering Mechanism Operational Test
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(25)
