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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. Actuator Installation
SUBTASK 27-61-51-420-001
(1) If it is necessary, install the unions [13] in the actuator [15]:
(a) Apply fluid, D00153 to the o-rings [14].
(b) Remove the caps from the hydraulic ports.
(c) Install the o-rings [14] and the unions [13] in the actuator [15].
SUBTASK 27-61-51-420-002
(2) Install the actuator [15]:
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(a) Remove the plugs from the hydraulic lines [12].
(b) Put the actuator [15] in its position and make sure the hydraulic lines [12] align with the
fittings.
(c) Loosely install the hydraulic lines [12] to the actuator [15].
(d) Connect the actuator [15] to the structure:
CAUTION: MAKE SURE YOU DO NOT INSTALL A WASHER ON THE SHORT TOP BOLT
[18]. THE BOLT [18] CAN TOUCH THE ACTUATOR [15] DURING THE
OPERATION OF THE ACTUATOR [15]. YOU CAN CAUSE DAMAGE TO THE
ACTUATOR [15].
1) Install the bolt [18] without a washer.
2) Install the washer [20] and bolt [19].
3) Install the washers [22] and bolts [21].
4) Tighten bolts [21] to 225-275 pound-inches (25.4-31.0 newton-meters).
5) Tighten bolt [18] and bolt [19] to 450-550 pound-inches (50.8-62.1 newton-meters).
(e) Tighten the nut on the hydraulic lines [12] on the actuator [15].
(f) Install the bolt [18], washer [9], nut [10] and pin [11].
(g) Connect the actuator rod end [17] to the flight spoiler [16]:
1) Apply a layer of grease, D00633 to the outer diameter of pin [3].
2) Install pin [3], washer [6] and nut [7].
3) Tighten nut [7] to 540-660 pound-inches(61.0-74.6 newton-meters).
4) Install bolt [1], washer [2], washer [4], pin [5] and lockwire [23].
SUBTASK 27-61-51-860-010
(3) Do this task: Put the Spoiler Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-61-00-840-802.
SUBTASK 27-61-51-860-005
(4) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-51-860-006
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.
(5) Do this task: Spoiler Hydraulic Systems A and B Pressurization, TASK 27-61-00-800-801.
SUBTASK 27-61-51-870-001
(6) Move the speed brake control lever through its full cycle to bleed the spoiler actuators.
SUBTASK 27-61-51-700-001
(7) Make sure there are no leaks at the hydraulic lines.
SUBTASK 27-61-51-820-001
(8) Do this task: Flight Spoiler Adjustment, TASK 27-61-00-820-803.
SUBTASK 27-61-51-820-002
(9) Do this task: Spoiler Actuator Linkage Adjustment, TASK 27-61-00-820-804.
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SUBTASK 27-61-51-730-001
(10) Do this task: Flight Spoiler System Test (Alternate Method), TASK 27-61-00-000-801.
E. Put the Airplane Back to Its Usual Condition.
SUBTASK 27-61-51-860-007
(1) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
SUBTASK 27-61-51-860-008
(2) 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 27-61-51-610-001
(3) Fill the hydraulic reservoirs if it is necessary. To fill, do this task: Hydraulic Reservoir
Servicing, TASK 12-12-00-610-801.
------------------------- END OF TASK ---------------------------
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FLIGHT SPOILER ACTUATOR - INSPECTION/CHECK
1. General
A. This task supplies the data for a dimensional inspection of the flight spoiler actuator.
B. This task does not remove or install the flight spoiler actuator, refer to the Flight Spoiler Actuator -
　
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