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system A. Electric pump 1 heat exchanger is installed in the fuel tank 2. Electric pump 2 heat
exchanger is installed in the fuel tank 1.
D. This procedure operates the electric hydraulic system A or B pumps to pressurize the hydraulic
systems A and B. Pressurization of the hydraulic systems with the engine-driven hydraulic pumps is
not included in this procedure.
TASK 27-61-00-800-801
2. Spoiler Hydraulic Systems A and B Pressurization
(Figure 201)
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)
32-00-01-480-801 Landing Gear Downlock Pins Installation (P/B 201)
B. Location Zones
Zone Area
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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
C. Procedure
SUBTASK 27-61-00-860-001
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-61-00-860-055
CAUTION: DO NOT OPERATE THE SYSTEM A OR B HYDRAULIC PUMPS FOR MORE THAN TWO
MINUTES WITHOUT FUEL IN THE FUEL TANKS. THE NO. 1 (FOR SYSTEM A) AND NO.
2 (FOR SYSTEM B) FUEL TANKS MUST HAVE A MINIMUM OF 250 GALLONS (1675
POUNDS/760 KILOGRAMS) OF FUEL IN THEM. IF THERE IS NOT SUFFICIENT FUEL IN
THE FUEL TANKS, THE HYDRAULIC SYSTEMS WILL BECOME TOO HOT.
(2) Make sure the No. 1 and No. 2 fuel tanks each have 250 gallons (1675 pounds/760 kilograms) of
fuel in them.
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SUBTASK 27-61-00-210-001
(3) Make sure the hydraulic reservoirs are full. To fill it, do this task: Hydraulic Reservoir
Servicing, TASK 12-12-00-610-801.
SUBTASK 27-61-00-860-002
(4) Make sure that this circuit breaker is closed:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 12 C00204 FLIGHT CONTROL SHUTOFF VALVES SPOILER
SUBTASK 27-61-00-860-003
(5) Set the parking brake.
SUBTASK 27-61-00-480-001
WARNING: MAKE SURE THAT THE GROUND LOCKS ARE INSTALLED IN ALL OF THE LANDING
GEAR BEFORE YOU PRESSURIZE THE HYDRAULIC SYSTEMS. WITHOUT THE
GROUND LOCKS, THE LANDING GEAR CAN RETRACT AND CAUSE INJURIES TO
PERSONS AND DAMAGE TO EQUIPMENT.
(6) Install the ground lock assemblies in the nose gear. To install them, do this task: Landing Gear
Downlock Pins Installation, TASK 32-00-01-480-801.
SUBTASK 27-61-00-860-004
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL SURFACES.
THESE COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC
POWER. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(7) Pressurize the spoiler hydraulic systems A and B:
(a) Set the ELEC 2, HYD PUMPS A or ELEC 1, HYD PUMPS B switch on the forward overhead
panel to the ON position.
(b) To pressurize the hydraulic system A, set the SPOILER A switch on the forward overhead
panel to the ON position.
(c) To pressurize the hydraulic system B, set the SPOILER B switch on the forward overhead
panel to the ON position.
------------------------- END OF TASK ---------------------------
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Spoiler Power Control Switches
Figure 201/27-61-00-990-801
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TASK 27-61-00-840-801
3. Put the Spoiler Hydraulic systems A and B Back to the Condition Before the Pressurization
(Figure 201)
A. References
Reference Title
32-00-01-080-801 Landing Gear Downlock Pins Removal (P/B 201)
B. Location Zones
Zone Area
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
210 Subzone - Control Compartment - Body Station 178.00 to Body
Station 259.50
C. Procedure
SUBTASK 27-61-00-860-005
(1) Set the ELEC 2, HYD PUMPS A and the ELEC 1, HYD PUMPS B switches on the forward
overhead panel to the OFF position.
SUBTASK 27-61-00-860-006
(2) Set the SPOILER A and B switches on the forward overhead panel to the OFF position.
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(143)
