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Panels Required Position Degrees Actual Position Degrees
8 and 9 37 +/- 3
10 and 11 32 +/- 3
2, 3, 4, 5 Partially Raised Yes/ No
(i) Turn the captain’s control wheel counterclockwise to 87 degrees and hold.
(j) Measure and record the position of flight spoilers 2, 3, 4 and 5.
NOTE: If spoiler panels 2, 3, 4 and 5 do not move, use the calculated panel travel from
above instead.
(k) Make sure spoiler panels 8, 9, 10 and 11 are partially raised.
Table 512/27-61-00-993-823
Panels Required Position Degrees Actual Position Degrees
2 and 3 32 +/- 3
4 and 5 37 +/- 3
8, 9, 10, 11 Partially Raised Yes/ No
SUBTASK 27-61-00-860-108
(15) Do these steps to check for spoiler laydown:
(a) Put the control wheel back in the neutral or zero position.
(b) Move the speed brake lever to the DOWN postition.
(c) Make sure all spoiler panels are in the full down position.
SUBTASK 27-61-00-820-023
(16) Do these steps to test spoiler operation with one system hydraulic power.
(a) Turn off the System A hydraulic power by switching the SPOILER A switch on the forward
overhead panel to OFF.
(b) Move the speed brake lever to the full up position.
(c) Make sure spoilers 3, 5, 8 and 10 are fully up.
(d) Make sure spoilers 2, 4, 9 and 11 are fully down.
(e) Move the speed brake lever to the DOWN position.
(f) Change SPOILER A switch to ON and SPOILER B switch to OFF on the forward overhead
panel.
(g) Move the speedbrake lever to the full UP position.
(h) Make sure that spoilers 2, 4, 9 and 11 are fully up.
(i) Make sure that spoilers 3, 5, 8, and 10 are in the fully down position.
(j) Return the speed brake lever to the down position
(k) Make sure that all spoiler panels are down.
SUBTASK 27-61-00-480-019
(17) Restore the aircraft to its usual configuration.
(a) Position the SPOILER B switch on the forward overhead panel to ON.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-61-00-860-109
(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.
SUBTASK 27-61-00-080-012
(2) Remove the mount, SPL-1670 and the control column assembly protractor, SPL-1680 from the
captain’s aileron control wheel.
SUBTASK 27-61-00-080-013
(3) Remove the protractor, COM-1691 from the spoilers No. 2, 3, 4, 5, 8, 9, 10 and 11.
------------------------- END OF TASK ---------------------------
TASK 27-61-00-000-802
11. Spoiler Manual Operation Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
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. 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
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-1691 Protractor - Digital, Vertical or Horizontal
(Part #: KS5549, Supplier: 75245, A/P Effectivity: 737-ALL)
C. Location Zones
Zone Area
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
D. Prepare for the Test
SUBTASK 27-61-00-860-065
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-61-00-860-066
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.
(2) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
SUBTASK 27-61-00-860-067
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737-600-700-800-900 飞机维护手册6 AIRCRAFT MAINTENANCE MANUA(20)
