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actuators through the spoiler mixer. The speed brake signals also control the ground spoilers.
C. You must not use the decals installed on the aileron control wheels during the adjustment or the test
of the spoiler control system. The decals are for flight crew use only.
TASK 27-61-00-710-801
2. Spoiler Control System Operational Test
A. References
Reference Title
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
B. Location Zones
Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
737-600/700/800/900
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C. Prepare for the Test
SUBTASK 27-61-00-860-014
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: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
D. Spoiler Control System Operational Test
SUBTASK 27-61-00-020-001
(1) Turn the captain’s aileron control wheel fully clockwise.
(a) Make sure the No. 8, 9, 10, and 11 flight spoilers move to the up position.
SUBTASK 27-61-00-020-002
(2) Turn the captain’s aileron control wheel fully counterclockwise.
(a) Make sure the No. 2, 3, 4 and 5 flight spoilers move to the up position.
SUBTASK 27-61-00-020-003
(3) Turn the captain’s aileron control wheel to the neutral position.
(a) Make sure the flight spoilers move to the retracted position.
SUBTASK 27-61-00-020-004
(4) Move the speed brake lever from the DOWN position to the UP position.
(a) Make sure the spoilers move to the UP position.
SUBTASK 27-61-00-020-005
(5) Move the speed brake lever from the UP position to the DOWN position.
(a) Make sure the flight spoilers move to the retracted position.
E. Put the Airplane Back to Its Usual Condition
SUBTASK 27-61-00-410-001
(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 ---------------------------
TASK 27-61-00-820-801
3. Spoiler Control Cables Adjustment
(Figure 501)
A. General
(1) Before you do cable adjustment, permit a minimum of one hour at a constant ambient
temperature of ±58F for the airframe temperature to become stable.
(a) The cable tension values will not be correct when there are temperature differences along
the cable run.
737-600/700/800/900
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B. References
Reference Title
27-61-00-800-802 Remove Pressure from the Spoiler Hydraulic Systems A and B
(P/B 201)
27-61-00-840-802 Put the Spoiler Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
C. 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-1554 Tensiometer - Cable (40-600 LB)
(Part #: ACM-600, Supplier: 13331, A/P Effectivity: 737-ALL)
(Part #: T60 1001-C9-1A, Supplier: 0N8U4, A/P Effectivity: 737-ALL)
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
SPL-1671 Straightedge - Control Wheel
(Part #: SE27-0001, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
D. Consumable Materials
Reference Description Specification
G00370 Tape - Lacing And Tying (Nylon) A-A-52080
E. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
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
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