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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Ground Spoiler Interlock Valve Installation
Figure 401 (Sheet 1 of 3)/27-62-61-990-801
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Ground Spoiler Interlock Valve Installation
Figure 401 (Sheet 2 of 3)/27-62-61-990-801
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Ground Spoiler Interlock Valve Installation
Figure 401 (Sheet 3 of 3)/27-62-61-990-801
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TASK 27-62-61-400-801
3. Ground Spoiler Interlock Valve 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)
27-62-00-800-801 Speed Brake Hydraulic Systems A and B Pressurization (P/B 201)
27-62-00-820-803 Ground Spoiler Interlock Valve Adjustment (P/B 501)
27-62-00-820-811 Ground Spoiler Interlock Valve Adjustment (Alternate Method)
(P/B 501)
27-62-00-840-801 Put the Speed Brake Hydraulic systems A and B Back to the
Condition Before the Pressurization (P/B 201)
27-62-00-840-802 Put the Speed Brake Systems A and B Back to the Condition Before
the Pressure Removal (P/B 201)
SWPM 20-60-03 Standard Wiring Practices Manual
B. Consumable Materials
Reference Description Specification
D00633 Grease - Aircraft General Purpose BMS3-33
G50171 Compound - Corrosion Inhibiting Compound,
Interior Application - D5026NS or ZC-026
C. Location Zones
Zone Area
134 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Right
D. Ground Spoiler Interlock Valve Installation
SUBTASK 27-62-61-800-001
(1) Make sure the valve [1] moves smoothly through its full travel.
SUBTASK 27-62-61-420-001
(2) Install the valve [1]:
(a) Install the reducers [13] and packings [14] in the ports of the valve [1]:
1) Remove the caps from the valve [1] ports.
2) Apply a thin layer of grease, D00633 on the packings [14].
3) Install the packings [14] and reducers [13] in the ports.
(b) Put the valve [1] in its position with the hydraulic lines [12] and ports aligned.
(c) Attach the valve [1] with washers [4] and bolts [3].
(d) Remove the plugs from the hydraulic lines [12].
(e) Connect the hydraulic lines [12] to the valve [1].
(f) Before you connect the electrical connector [2] and electrical connector [5], examine the
connectors for corrosion.
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WARNING: DO THE STEPS BELOW IF THE AIRPLANE OPERATES AT AIRPORTS WHERE
DEICING FLUID THAT CONTAIN POTASSIUM FORMATE IS USED. ALSO DO THE
STEPS FOR ALL AIRPLANES THAT YOU FOUND CORROSION IN THE
ELECTRICAL CONNECTORS IN THE MAIN WHEEL WELL. THE ELECTRICAL
CONNECTOR IS PART OF A SYSTEM THAT IS NECESSARY FOR SAFE FLIGHT.
(g) If there was corrosion, refer to (SWPM 20-60-03) to correct the problem.
(h) Apply the D5026NS or ZC-026 compound, G50171 to the connectors (SWPM 20-60-03).
(i) Connect the electrical connector [5] and the electrical connector [2].
(j) Install bolt [7], washer [8], washer [9], and nut [10] to connect the push-pull cable [6] to the
valve input lever [11].
SUBTASK 27-62-61-860-002
(3) 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 27-62-61-860-003
(4) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-62-61-860-004
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: Speed Brake Hydraulic Systems A and B Pressurization,
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(18)
