曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

24-22-00-860-811 Supply Electrical Power (P/B 201)
24-22-00-860-812 Remove Electrical Power (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-61-00-800-802 Remove Pressure from the Spoiler Hydraulic Systems A and B
(P/B 201)
B. Tools/Equipment
Reference Description
STD-1110 Container - Hydraulic Fluid Resistant, 5 Gallon (19 Liters)
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 Removal
SUBTASK 27-61-51-860-001
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-51-860-003
(2) Do this task: Extend the Trailing Edge Flaps, TASK 27-51-00-860-803.
SUBTASK 27-61-51-860-009
(3) To remove hydraulic power from the spoiler system, do this task: Remove Pressure from the
Spoiler Hydraulic Systems A and B, TASK 27-61-00-800-802.
SUBTASK 27-61-51-862-001
(4) Do this task: Remove Electrical Power, TASK 24-22-00-860-812.
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E. Actuator Removal
SUBTASK 27-61-51-020-001
(1) Disconnect the hydraulic lines [12] from the actuator [15].
(a) Put a 5 gallon (19 liters) hydraulic fluid resistant container, STD-1110 below the actuator [15]
to catch the hydraulic fluid.
(b) Disconnect the hydraulic lines [12] from the actuator [15].
(c) Install the plugs in the hydraulic lines [12].
SUBTASK 27-61-51-020-002
(2) Disconnect the actuator rod end [17] from the flight spoiler [16]:
(a) Remove the bolt [1], washer [2], lockwire [23], pin [5] and washer [4] from the actuator rod
end [17].
(b) Remove nut [7], washer [6] and pin [3] that attach the actuator rod end [17] to the flight
spoiler [16].
SUBTASK 27-61-51-020-011
(3) Remove the pin [11], nut [10], washer [9], and bolt [8].
SUBTASK 27-61-51-020-003
(4) Disconnect the actuator [15] from the structure:
(a) Remove the bolts [21] and washers [22].
(b) Remove the bolt [19] and washer [20].
(c) Remove the bolt [18].
SUBTASK 27-61-51-020-005
(5) Remove the actuator [15] from the airplane.
SUBTASK 27-61-51-480-001
(6) If it is necessary, remove the unions [13] and o-rings [14] from the actuator [15].
(a) Install caps in the ports of the actuator [15].
------------------------- END OF TASK ---------------------------
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Flight Spoiler Actuator Installation
Figure 401 (Sheet 1 of 2)/27-61-51-990-801
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Flight Spoiler Actuator Installation
Figure 401 (Sheet 2 of 2)/27-61-51-990-801
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TASK 27-61-51-400-801
3. Flight Spoiler Actuator Installation
(Figure 401)
A. References
Reference Title
12-12-00-610-801 Hydraulic Reservoir Servicing (P/B 301)
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-61-00-000-801 Flight Spoiler System Test (Alternate Method) (P/B 501)
27-61-00-800-801 Spoiler Hydraulic Systems A and B Pressurization (P/B 201)
27-61-00-820-803 Flight Spoiler Adjustment (P/B 501)
27-61-00-820-804 Spoiler Actuator Linkage Adjustment (P/B 501)
27-61-00-840-801 Put the Spoiler Hydraulic systems A and B Back to the Condition
Before the Pressurization (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)
B. Consumable Materials
Reference Description Specification
D00153 Fluid - Hydraulic, Erosion Arresting, Fire Resistant BMS3-11, Type
IV
(interchange~
able&
intermixable
with Type V)
D00633 Grease - Aircraft General Purpose BMS3-33
　
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