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Zone Area
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
566 Left Wing - Spoiler No. 1
666 Right Wing - Spoiler No. 12
E. Actuator Installation
SUBTASK 27-62-94-420-001
(1) Connect the hydraulic lines [9]:
(a) Remove the caps from the hydraulic ports.
(b) Apply MCS 352B fluid, D00054 or fluid, D00153 to the packing [16], packing [17], union [15]
and restrictor [18].
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(c) Install the packing [16], packing [17], union [15], and restrictor [18] in the actuator
assembly [10].
SUBTASK 27-62-94-420-002
(2) Install the actuator assembly [10]:
(a) Put the actuator assembly [10] in its position and make sure the hydraulic lines [9] align
with the fittings.
(b) Install pillow blocks [11] on the actuator assembly [10]:
1) Apply grease, D00633 to the split ball bearings [12].
2) Assemble the split ball bearings [12].
3) Install split ball bearings [12] in pillow blocks [11].
4) Make sure the split ball bearings [12] move freely.
5) Apply compound, C00913 to the bolts [13].
6) Install the bolts [13] and washers [14].
7) Tighten the bolts [13] to 225-275 pounds-inches (25.4-31.1 newton-meters).
(c) Connect the piston rod to the ground spoiler [1]:
1) Apply grease, D00633 to all surfaces of the bolt [2], bushing [4] and bushing [5].
2) Install the bolt [2], washer [3], bushing [4], bushing [5] washer [6], nut [7] and pin [8] in
the piston rod.
3) Tighten the nut [7] to 660-780 pound-inches (74.6-88.1 newton-meters).
SUBTASK 27-62-94-420-003
(3) Connect the hydraulic lines [9] to the actuator assembly [10]:
(a) Remove the plugs from the hydraulic lines [9].
(b) Connect the hydraulic lines [9] to the actuator assembly [10].
(c) Tighten the hydraulic fittings.
SUBTASK 27-62-94-860-007
(4) Do this task: Put the Speed Brake Systems A and B Back to the Condition Before the
Pressure Removal, TASK 27-62-00-840-802.
SUBTASK 27-62-94-860-008
(5) Do this task: Speed Brake Hydraulic Systems A and B Pressurization,
TASK 27-62-00-800-801.
SUBTASK 27-62-94-870-001
(6) Move the speed brake control lever to bleed the spoiler actuators.
SUBTASK 27-62-94-700-001
(7) Make sure there is no leakage of hydraulic fluid at the actuator assembly [10].
SUBTASK 27-62-94-820-001
(8) Do this task: Ground Spoiler Adjustment, TASK 27-62-00-820-804.
SUBTASK 27-62-94-820-002
(9) Do this task: Outboard Ground Spoiler Test, TASK 27-62-91-000-802.
F. Put the Airplane Back to Its Usual Condition.
SUBTASK 27-62-94-860-009
(1) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
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SUBTASK 27-62-94-860-010
(2) Move the speed brake lever to the DOWN position to the lower the spoilers.
SUBTASK 27-62-94-860-011
(3) Do this task: Put the Speed Brake Hydraulic systems A and B Back to the Condition Before
the Pressurization, TASK 27-62-00-840-801.
SUBTASK 27-62-94-860-012
(4) Put the SPOILER A and B switches in the ON position.
------------------------- END OF TASK ---------------------------
TASK 27-62-94-000-802
4. Outboard Ground Spoiler Actuator Test
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (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)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B 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
566 Left Wing - Spoiler No. 1
666 Right Wing - Spoiler No. 12
D. Prepare for the Test
SUBTASK 27-62-94-860-013
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-62-94-860-014
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
　
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